{"Affiliation":[{"label":"Affiliation","value":"Science, Faculty of","attrs":{"lang":"en","ns":"http:\/\/vivoweb.org\/ontology\/core#departmentOrSchool","classmap":"vivo:EducationalProcess","property":"vivo:departmentOrSchool"},"iri":"http:\/\/vivoweb.org\/ontology\/core#departmentOrSchool","explain":"VIVO-ISF Ontology V1.6 Property; The department or school name within institution; Not intended to be an institution name."},{"label":"Affiliation","value":"Physics and Astronomy, Department of","attrs":{"lang":"en","ns":"http:\/\/vivoweb.org\/ontology\/core#departmentOrSchool","classmap":"vivo:EducationalProcess","property":"vivo:departmentOrSchool"},"iri":"http:\/\/vivoweb.org\/ontology\/core#departmentOrSchool","explain":"VIVO-ISF Ontology V1.6 Property; The department or school name within institution; Not intended to be an institution name."}],"AggregatedSourceRepository":[{"label":"Aggregated Source Repository","value":"DSpace","attrs":{"lang":"en","ns":"http:\/\/www.europeana.eu\/schemas\/edm\/dataProvider","classmap":"ore:Aggregation","property":"edm:dataProvider"},"iri":"http:\/\/www.europeana.eu\/schemas\/edm\/dataProvider","explain":"A Europeana Data Model Property; The name or identifier of the organization who contributes data indirectly to an aggregation service (e.g. Europeana)"}],"Campus":[{"label":"Campus","value":"UBCV","attrs":{"lang":"en","ns":"https:\/\/open.library.ubc.ca\/terms#degreeCampus","classmap":"oc:ThesisDescription","property":"oc:degreeCampus"},"iri":"https:\/\/open.library.ubc.ca\/terms#degreeCampus","explain":"UBC Open Collections Metadata Components; Local Field; Identifies the name of the campus from which the graduate completed their degree."}],"Creator":[{"label":"Creator","value":"MacDonald, Jack Robert","attrs":{"lang":"en","ns":"http:\/\/purl.org\/dc\/terms\/creator","classmap":"dpla:SourceResource","property":"dcterms:creator"},"iri":"http:\/\/purl.org\/dc\/terms\/creator","explain":"A Dublin Core Terms Property; An entity primarily responsible for making the resource.; Examples of a Contributor include a person, an organization, or a service."}],"DateAvailable":[{"label":"Date Available","value":"2011-10-20T18:05:18Z","attrs":{"lang":"en","ns":"http:\/\/purl.org\/dc\/terms\/issued","classmap":"edm:WebResource","property":"dcterms:issued"},"iri":"http:\/\/purl.org\/dc\/terms\/issued","explain":"A Dublin Core Terms Property; Date of formal issuance (e.g., publication) of the resource."}],"DateIssued":[{"label":"Date Issued","value":"1964","attrs":{"lang":"en","ns":"http:\/\/purl.org\/dc\/terms\/issued","classmap":"oc:SourceResource","property":"dcterms:issued"},"iri":"http:\/\/purl.org\/dc\/terms\/issued","explain":"A Dublin Core Terms Property; Date of formal issuance (e.g., publication) of the resource."}],"Degree":[{"label":"Degree (Theses)","value":"Doctor of Philosophy - PhD","attrs":{"lang":"en","ns":"http:\/\/vivoweb.org\/ontology\/core#relatedDegree","classmap":"vivo:ThesisDegree","property":"vivo:relatedDegree"},"iri":"http:\/\/vivoweb.org\/ontology\/core#relatedDegree","explain":"VIVO-ISF Ontology V1.6 Property; The thesis degree; Extended Property specified by UBC, as per https:\/\/wiki.duraspace.org\/display\/VIVO\/Ontology+Editor%27s+Guide"}],"DegreeGrantor":[{"label":"Degree Grantor","value":"University of British Columbia","attrs":{"lang":"en","ns":"https:\/\/open.library.ubc.ca\/terms#degreeGrantor","classmap":"oc:ThesisDescription","property":"oc:degreeGrantor"},"iri":"https:\/\/open.library.ubc.ca\/terms#degreeGrantor","explain":"UBC Open Collections Metadata Components; Local Field; Indicates the institution where thesis was granted."}],"Description":[{"label":"Description","value":"The cross section for the photodisintegration of helium-3 has been measured at gamma ray energies of 8.06 and 9.17 mev.  The He\u00b3 (\u0263,p)D reaction cross section at 8.06 and 9.17 mev  was found to be 0.493\u00b1 0.066 and 0.723\u00b1 0.087 millibarns respectively.  The He\u00b3 (\u0263,n)2p reaction cross section at 9.17 mev  was found to be 0.25\u00b1  0.13 millibarns. These results are compared with other experimental work on the photodisintegration of helium-3 and tritium.\r\nThe photodisintegration reaction was observed in a cylindrical gridded ionization chamber using a helium-3,  methane, and argon gas mixture.  The C\u00b9\u00b3 (p,\u0263) N\u00b9\u2074  reactions at proton bombarding energies of 0.554 and 1.75 mev were used as the source of gamma rays of well defined energy. The preparation of carbon-13 targets is discussed in detail.\r\nTheoretical calculations on the photodisintegration of mass 3 nuclei are summarized.  Photodisintegration and electron scattering measurements are compared as methods of determining the nature of the ground state wave function of the mass 3 system.","attrs":{"lang":"en","ns":"http:\/\/purl.org\/dc\/terms\/description","classmap":"dpla:SourceResource","property":"dcterms:description"},"iri":"http:\/\/purl.org\/dc\/terms\/description","explain":"A Dublin Core Terms Property; An account of the resource.; Description may include but is not limited to: an abstract, a table of contents, a graphical representation, or a free-text account of the resource."}],"DigitalResourceOriginalRecord":[{"label":"Digital Resource Original Record","value":"https:\/\/circle.library.ubc.ca\/rest\/handle\/2429\/38126?expand=metadata","attrs":{"lang":"en","ns":"http:\/\/www.europeana.eu\/schemas\/edm\/aggregatedCHO","classmap":"ore:Aggregation","property":"edm:aggregatedCHO"},"iri":"http:\/\/www.europeana.eu\/schemas\/edm\/aggregatedCHO","explain":"A Europeana Data Model Property; The identifier of the source object, e.g. the Mona Lisa itself. This could be a full linked open date URI or an internal identifier"}],"FullText":[{"label":"Full Text","value":"THE PHOTODISINTEGRATION OF HELIUM-3 AT PHOTON ENERGIES OF 8.06 AND 9.17 MEV JACK ROBERT MACDONALD B.A.Sc\u2022, The U n i v e r s i t y of B r i t i s h Columbia, 1960 A THESIS SUBMITTED IN PARTIAL FULFILMENT OF THE REQUIREMENTS FOR THE DEGREE OF DOCTOR OF PHILOSOPHY i n the Department of PHYSICS We accept th i s thesis as conforming to the required standard THE UNIVERSITY OF BRITISH COLUMBIA September 1964 In p r e s e n t i n g t h i s t h e s i s i n p a r t i a l f u l f i l m e n t of the requirements f o r an advanced degree at the U n i v e r s i t y of B r i t i s h Columbia, I agree that the L i b r a r y s h a l l make i t f r e e l y a v a i l a b l e f o r r e f e r e n c e and study, I f u r t h e r agree that per-m i s s i o n f o r extensive copying of t h i s t h e s i s f o r s c h o l a r l y purposes may be granted by the Head of my Department or by h i s r e p r e s e n t a t i v e s . I t i s understood t h a t , c o p y i n g or p u b l i -c a t i o n of t h i s t h e s i s f o r f i n a n c i a l gain s h a l l not be allowed without my w r i t t e n permission.-, Department of The U n i v e r s i t y of B r i t i s h Columbia, Vancouver 8 f Canada Date O C T ^ g ^ ~7 , (^4 The University of B r i t i s h Columbia FACULTY OF GRADUATE STUDIES PROGRAMME OF THE FINAL ORAL EXAMINATION FOB, THE DEGREE OF DOCTOR OF PHILOSOPHY B \u201e A \u201e S c c j The Univ e r s i t y of B r i t i s h Columbia* 1960 TUESDAY, OCTOBER 6, 1964, AT 3;-00 P.M. ROOM 12, HEBB BUILDING, (PHYSICS) COMMITTEE IN CHARGE Chairman; I. McT. Cowan of JACK ROBERT MACDONALD W . M o Armstrong K. L\u00bb Erdman C. Froese. D,\u201eL..Livesey J o Mo McMillan J . Bo Warren External Examiner: Leon Katz Department of Physics University of Saskatchewan THE PHOTODISINTEGBATION OF HELIUM-3 AT PHOTON ENERGIES OF 8.06 AM) 9,17 MEV. ABSTRACT The cross section f o r the photodisintegration of helium-3 has been measured at. gamma ray energies of 8,06 and 9.17 mev. The He 3 (<JN,p)D reaction cross section at 8,06 and 9.17 mev was found t.o be 0,493 t 0.066 and 0,723 t 0,087 m i l l i b a r n s r e s p e c t i v e l y . The He 3 ,n)2p reaction cross section at 9,17 mev was found to be 0.25 i 0,13 m i l l i b a r n s . These r e s u l t s are compared with other experimental work on the photodisintegration of helium-3 and t r i t i u m . The photodisintegration reaction was observed i n a c y l i n d r i c a l gridded i o n i z a t i o n chamber using a helium-3^  methane, and argon gas mixture. The, C^3(p s y )_t\\jl4 reactions at proton bombarding energies of 0,554 and 1.75 mev were used as the source, of gamma rays of well defined energy. The preparation of carbon-13 targets i s discussed i n d e t a i l . T heoretical c a l c u l a t i o n s on the photodisintegration of mass 3 n u c l e i are summarized, Photodisintegration and electron s c a t t e r i n g measurements are compared as, methods of determining the nature of the ground state wave function of the mass 3 system. GRADUATE STUDIES F i e l d of Study: Physics Electromagnetic Theory Waves Nuclear Physics Elementary Quantum. Mechanics Nuclear Reactions S o l i d State Physics Special R e l a t i v i t y Theory Introduction to Low Temperature Physics Group Theory Methods~ Theoretical Nuclear Physics Advanced Quantum Mechanics Related Studies: Numerical Analys i s E l e c t r o n i c Instrumentation G.M, Volkoff .J.G, Savage J.B. Warren W, Opechowski B tL, White R, Barrie W, Opechowski D.V, Osborne W. Opechowski P,D, Kunz P, Rastall T.E,. Hull F.K, Bowers PUBLICATIONS Gas Flow Regulator for an r f Ion Source, Rev. S c i . Inst. 33, 1111 (1962) Removal of Tritium from Helium-3, Rev. S c i . Inst. 34, 1280 (1963) Photodisintegration of Helium-3, B u l l . Amer. Phys,, Soc. 8, 124 (1963) Photodisintegration of Helium-*3 near the threshold, Phys. Rev. 132, 1691 (1963) Simple Gas C i r c u l a t i o n Pump, Rev. S c i . Inst. 35, 241 (1964) Simple Electron Bombardment Apparatus f or Evaporating Boron, Rev. S c i . Inst. 35, 122 (1964) - i -ABSTRACT The cross section f o r the photodisintegration of helium-3 has been measured at gamma ray energies of 8.06 and 9.17 mev. The He (\u00a3,p)D reaction cross section at 8.06 and 9.17 mev was found to be 0.493 \u00b1 0.066 and 0.723 \u00b1 0.087 m i l l i b a r n s r e s p e c t i v e l y . The He (tf,n)2p reaction cross section at 9.17 mev was found to be 0.25 \u00b1 0.13 m i l l i b a r n s . These r e s u l t s are compared with other experimental work on the photodisintegration of helium-3 and t r i t i u m . The photodisintegration reaction was observed i n a c y l i n d r i c a l gridded i o n i z a t i o n chamber using a helium-3, methane, and argon gas mixture. The C 1 3 ( p , ^ ) N 1 4 reactions at proton bombarding energies of 0.554 and 1.75 mev were used as the source of gamma rays of well defined energy. The preparation of carbon-13 targets i s discussed i n d e t a i l . Theoretical calculations on the photodisintegration of mass 3 n u c l e i are summarized. Photodisintegration and electron scattering measurements are compared as methods of determining the nature of the ground state wave function of the mass 3 system. - i i -TABLE OF CONTENTS Page Chapter I - INTRODUCTION 1 Chapter I I - THEORETICAL ESTIMATES OF THE CROSS SECTION FOR THE PHOTODISINTEGRATION OF HELIUM-3 ... 4 A. Reaction Kinematics 4 B. Theoretical Estimates of the Cross Section 5 Chapter III - PHOTODISINTEGRATION OF 3-BODY NUCLEI-EXPERIMENTAL RESULTS 10 Chapter IY - APPARATUS AND EXPERIMENTAL ARRANGEMENT FOR THE PHOTODISINTEGRATION MEASUREMENT 17 A. Introduction 17 B. C y l i n d r i c a l Gridded Ionization Chamber 17 1. Chamber Operation 17 2. Chamber Construction 18 3. Gas Mixtures 20 C. Energy C a l i b r a t i o n of the Chamber 23 D. Chamber Background 27 E. Pulse Amplification and Analysis 29 F. Gramma Flux Measurement 30 G. Experimental Arrangement 31 Chapter V - PHOTODISINTEGRATION RESULTS AND ESTIMATION OF THE CROSS SECTION AT 8.06 AND 9.17 MEV.. 33 A. Spectrum at 8.06 mev 33 B. Spectrum at 9.17 mev - 2-body Breakup 33 C. Spectrum at 9.17 mev - 3-body Breakup 34 D. Analysis of the 2-body Data 35 E. Cross Section Calculation f o r the Reaction He3()r,p)D 36 - i i i -Page Chapter Y (cont) F. Errors i n the 2-body Cross Section 36 G. Estimation of the He3()T,n)2p Cross Section 38 Chapter 71 - DISCUSSION OF EXPERIMENTAL MEASUREMENTS AND THEORETICAL CALCULATIONS ON THE 3-NUCLEON SYSTEM 39 A. Photodisintegration of Helium-3 39 B. Theoretical Cross Section Calculations 42 C. Electron Scattering on Tritium and Helium-3 43 D. Conclusions 45 Appendix A - CROSS SECTION CALCULATIONS 47 A. Chamber E f f i c i e n c y 47 B. Atom Density of Helium-3 49 C. Wall E f f e c t 50 1. Wall Loss 50 2. Spectrum Shape due to the Wall Loss 51 3. 2-body Photodisintegration Spectrum Analysis .... 53 Appendix B - THE PREPARATION OF CARBON-13 TARGETS 56 Appendix C - THE REACTION C 1 3 ( p , t t ) N 1 4 AND THE MEASURE-MENT OF THE GAMMA FLUX V. 60 A. Gamma Ray Counter E f f i c i e n c y 60 B. The Reaction C 1 3 ( p , t t ) N 1 4 as a Source of Gamma Rays 61 \u2022 1. Introduction 61 2. 0.554 mev Resonance 62 3. 1.75 mev Resonance 63 4. Doppler S h i f t 64 C. Analysis of the Gamma Spectra 65 1. 0.554 mev Resonance 65 - i v -Appendix C (cont) Page 2. 1.75 mev Resonance 67 Appendix D - NEUTRON INDUCED BACKGROUND AND NEUTRON SHIELDING 69 Appendix E - PHOTODISINTEGRATION OE HE 3 NEAR THE THRESHOLD by J. B. Warren, K. L. Erdman, L. P. Robertson, D. A. Axen, and J . R. MacDonald reprinted from The Physical Review, 132, 1691 (1963) following p.72 Appendix F - GAS FLOW REGULATOR FOR AN r f ION SOURCE, by B. L. White, L. P. Robertson, K. L. Erdman, and I. R. MacDonald reprinted from The Review of S c i e n t i f i c Instruments, 33, 1111 (1962) following p.72 Appendix G - REMOVAL OF TRITIUM FROM HE 3 by K. L. Erdman, L. P. Robertson, D. Axen, and J . R. MacDonald reprinted from The Review of S c i e n t i f i c Instruments, 34, 1280(1963).. following p.72 Appendix H - SIMPLE GAS CIRCULATION PUMP by K. L. Erdman J . R. MacDonald, G. A. Beer, and D. A. Axen reprinted from The Review of S c i e n t i f i c Instruments, 35, 241 (1964) .... following p.72 Appendix I - SIMPLE ELECTRON BOMBARDMENT APPARATUS FOR EVAPORATING BORON by K. L. Erdman, D. Axen J. R. MacDonald, and L. P. Robertson reprinted from The Review of S c i e n t i f i c Instruments, 35, 122 (1964) .... following p.72 Appendix J - PHOTODISINTEGRATION OF ARG0N-40 AT 9.17 AND 17.7 MEV by M. A. Reimann, J . R. MacDonald, and I. B. Warren, preprint of a r t i c l e to be published i n Nuclear Physics, (1964) following p.72 Bibliography 73 -v-LIST OF FIGURES to follow page 1. Energy D i s t r i b u t i o n f o r the Sum of the Energies of the Two Protons f o r the Reaction H e 3 ^ ,n)2p ....... 5 2. Theoretical Estimates of the Cross Section f o r the Reaction He 3( t ,p)D 7 3. Theoretical Estimates of the Cross Section f o r the Reaction He^Of ,n)2p 7 4. H e 3 ( t ,p)D and T ( t ,n)D Cross Sections from Eichmann (1963) 8 5. He 3()f ,p)D D i f f e r e n t i a l Cross Section at 90\u00b0 i n the Laboratory System 11 6. Cross Sections f o r the Reactions He 3(Y*p)D and He 3()f ,n)2p from Gorbunov and Varfolomeev (1964) .... 14 7. Ionization Chamber 18 8. D e t a i l s of Co l l e c t o r Support 19 9. Electrode Voltage Supply 19 10. Charged P a r t i c l e Ranges i n Gases 20 11. E f f e c t of P u r i f i c a t i o n on Voltage Pulse Amplitude ... 24 12. Chamber Energy C a l i b r a t i o n 27 13. Chamber Background 29 14. Experimental Arrangement 31 15. Photodisintegration Spectrum, 8.06 mev Gamma Rays ... 33 16. Photodisintegration Spectrum f o r the Reaction He3(y,p)D at a Gamma Ray Energy of 9.17 mev 33 17. Photodisintegration Spectrum f o r the Reactions He 3( X ,n)2p and A 4 0 ( T ,\u00ab*)S35 at a Gamma Ray Energy of 9.17 mev 34 18. Cross Section f o r the Reactions He 3 (V,p)D and T(tf,n)D 36 - v i -to .follow page 19. Angular D i s t r i b u t i o n of the Reaction Products f o r the Reaction He3(}p,p)D .' 39 20. Comparison of Total and D i f f e r e n t i a l Cross Section Measurements 41 21. H 0 ( a ) vs. d and H 2(d)\/H 0(d) vs. d 49 22. Wall Loss Spectra f o r the Reaction He 3(tt ,p)D 52 23. Hypothetical Spectrum Shape due to Wall Loss 53 24. Target Preparation Apparatus 57 25. Y i e l d of 9.17 mev Gamma Rays as a Function of Proton Energy 58 26. Gamma Counter E f f i c i e n c y 60 27. Decay Schemes f o r the 8.06 and 9.17 mev Levels of N^-4 63 28. Gamma Spectrum from the Reaction C 1 3 ( p , tt ) N 1 4 at the 0.554 mev Resonance 65 29. 6.14 mev Gamma Spectrum from the Reaction F 1 9 ( p , e * ) f ) 0 1 6 at the 340 kev Resonance 66 30. Gamma Spectrum from the Reaction C 1 3 ( p , t t ) N 1 4 at the 1.75 mev Resonance 67 31. Cross Section f o r the Reaction He 3(n,p)T 69 32. Beam Collimators and Neutron Shielding 70 - v i i -LIST 0? TABLES to follow page I 90\u00b0 Differential Cross, Section for He3()f,p)D from Bennan, Koester and Smith (1964) ... in text p.11 II 90\u00b0 Differential Cross Section for He3(2T,p)D from Stewart, Morrison and O^Connell (1964) in text p.13 III Cross Section for the Reaction T(tf,n)D .. in text p.16 IV Chamber Dimensions 18 V Chamber F i l l i n g s in text p.23 VI Alpha Particle Backgrounds in text p.28 VII Data from Photodisintegration Spectra for He3()T,p)D 35 VIII He3()f,p)D Cross Section Data 36 IX Estimate of Errors 36 X Cross Section Errors in text p.37 XI Data for 3-body Cross Section at 9.17 mev 38 XII Measured Angular Distribution of the 9.17 mev Radiation at the 1.75 mev Resonance in text p.63 XIII Angular Distributions, Relative Intensities, and. Sc i n t i l l a t i o n Counter Efficiencies .... to follow p.68 XIV (p,n) Thresholds to follow p.71 - v i i i -AC KNOWLEDGEMENTS I wish to express my sincere gratitude to Dr. K. L. Erdman f o r h i s kind supervision of t h i s research projeot and hi s w i l l i n g guidance throughout my research career. The assistance of Dr. J . B. Warren, Dr. B. L. White, Dr. G. M. G r i f f i t h s , Dr. G. Jones and Dr. M. McMillan proved invaluable and was greatly appreciated. I g r a t e f u l l y acknowledge the assistance of Dr. L. Robertson, Mr. D. Axen, Mr. M. Reimann and Mr. D. Healey i n operating the Van de Graaff and i n performing the measurements. Words f a i l to express my gratitude to my mother, my father and my wife f o r t h e i r endless patience and constant enc ouragement. I am deeply indebted to the National Research Council f o r the four scholarships held during the course of t h i s work. -1-CHAPTER I Introduction Nuclear photodlsintegration reactions involve the in t e r a c t i o n of the electromagnetic f i e l d of a photon with the charges, currents and e l e c t r i c and magnetic moments of a nucleus, which i n turn are calculated from the wave functions describing the nuclear system. As the inte r a c t i o n of el e c t r o -magnetic f i e l d s with charge systems i s well understood, the ca l c u l a t i o n of the ra d i a t i v e matrix elements and hence the reaction p r o b a b i l i t y or cross section only involves assumptions concerning the i n i t i a l and f i n a l state wave functions of the system. Furthermore, the knowledge gained about the wave functions through photodlsintegration experiments can i n pr i n -c i p l e be used to obtain information about the nuclear forces. The comparison between theory and experiment f o r the photodlsintegration of the deuteron served to test the basic theory of photonuclear reactions. Accounts of experimental data on the deuteron photo-effect can be found i n Wilkinson et a l (1952) and Hulthen and Sugawara (1957). The agreement between experiment and theory i s very good, l a r g e l y because the deuteron i s loosely bound. This allows the deuteron wave function to be well approximated by i t s known asymptotic form. Consideration of the photo-effect i n the 3-nucleon system leads to a considerable difference i n the methods of -2-t h e o r e t i c a l a n a l y s i s . F i r s t l y , the 3-nucleon system i s known to be t i g h t l y bound so that asymptotic wave functions may well be less r e l i a b l e than i n the case of the deuteron. Secondly, the wave functions for the ground state of the nucleus cannot be e a s i l y calculated from a p o t e n t i a l . As a f i r s t approximation, the wave functions used to date have generally been chosen to have an a n a l y t i c a l form which Is integrable. Usually these wave functions are j u s t i f i e d by assuming a p o t e n t i a l and c a l c u l a t i n g the binding energy of the system by a v a r i a t i o n a l method. Photo-d i s i n t e g r a t i o n cross sections f o r the 3-nucleon system have been calculated with some of these assumed wave functions. The cross sections are very sensitive to the assumed form of wave function. 1 The need f o r accurate cross section measurements of the photo-effect f o r a 3-nucleon, system i s obvious. Such measurements would supplement the experimental data of e l a s t i c scattering of electrons from t r i t i u m and helium -3 and provide the most sensitive test f o r 3-body wave functions. One's hope i s that these measurements w i l l give a more precise determina-t i o n of both i n i t i a l and f i n a l state 3-nucleon wave functions and perhaps y i e l d information about the nucleon-nucleon i n t e r -action, i f only as evidenced by the f i n a l state i n t e r a c t i o n . There would seem to be too many variables i n the problem to allow one to make d e f i n i t e statements about a possible 3-body force. In view of the need f o r such measurements, an experi-ment to measure the photodisintegration cross section for -3-helium-3 was begun at U.B.C. as early as 1958. The f i r s t measurements on helium-3 were reported by Warren et a l (1963). This thesis i s concerned with the extension of the e a r l i e r work to higher photon energies and a preliminary i n v e s t i g a t i o n of the 3 p a r t i c l e breakup of helium-3. Theoretical estimates of the cross section f o r the photodisintegration of the 3-nucleon system are discussed i n Chapter I I . A resume of the experimental work done i n other laboratories on the photo-effect i n hellum-3 and t r i t i u m i s given i n Chapter I I I . The U.B.C. measurements are discussed i n d e t a i l i n Chapters IY and Y and Appendix E. A comparison between theory and experiment Is given i n Chapter YI. -4-CHAPTER I I Theoretical Estimates of the Cross Section  for the Photodlsintegration of Helium-5 A. Reaction Kinematics For gamma ray energies below the pion production threshold, the possible photodlsintegration reactions of hellum-3 are He3 + * \u2014 \u2022 p \"D H e 3 ^ \u2014 \u2022 P + P + n The Q-values f o r the 2 and 3-body breakup, Q2 and Qg, calculated from the mass values given by Eve r l i n g et a l (I960) are Q 2 = -5.4-9316 \u00b1 O.OOOB3 ttev Q B - - 7. 7! 9 \u00b1 O.OOJ mev I f the momentum of the photon i s neglected, the proton and deuteron i n the 2-body breakup w i l l have w e l l defined f r a c t i o n s of the t o t a l energy E 0 = (E^ -5.493) mev For the 3-body photodlsintegration, a continuum energy spectrum w i l l be observed i f only one or two of the reaction products are detected. The sum of the energies of the two protons, E o t ) , extends from a minimum energy of EQ^ n= 1\/3 (E<\u00a3- 7.719) mev to a maximum energy of -5-max E o b = (E^, - 7.719) mev. The minimum observed energy corres-ponds to the two protons emitted i n the same d i r e c t i o n with equal energies. The maximum observed energy corresponds to the two protons being emitted i n opposite directions with the neutron having zero momentum. The observed energy d i s t r i b u t i o n w i l l depend on the density of f i n a l states of the reaction, and hence i s propor-t i o n a l to the volume i n phase space associated with the momen-tum d i s t r i b u t i o n of the three p a r t i c l e s . The p r o b a b i l i t y of a given momentum d i s t r i b u t i o n i s i n turn dependent upon the nuclear and coulomb interactions of the three p a r t i c l e s . Robertson (1963) derives the shape of the energy d i s t r i b u t i o n f o r the two protons i n the 3-body brealaip neglecting f i n a l state i n t e r a c t i o n s . Figure 1 shows this energy d i s t r i b u t i o n . Deviations from this spectrum shape can be attributed to f i n a l state i n t e r a c t i o n s . B. Theoretical Estimates of the Gross Section There have been f i v e calculations on the photodisin-tegration of the 3-nucleon systems, t r i t i u m and helium-3. The calculations of Verde (1950), Gunn and Irving (1951) and Rossetti (1959) are quite s i m i l a r and d i f f e r only i n the choice of the form of the ground state wave function. In each case, the assumed ground state wave function was an S-state, t o t a l l y symmetrical i n the s p a t i a l co-ordinates of a l l three nucleons. (It i\u00a3[ known, from magnetic moment data, that the t o t a l l y symmetric S-state component of the ground state wave function O-S l-O U 5 S U M O F -me E M E R S Y O F T H E T W O P R O T O N S R W * A t G M - U - I A \u00ab * Y E N E R G Y O F 9 - 1 7 M E V FIGURE 1 Energy Distribution for the Sum of the Energies of the Two Protons for the Reaction He3( Jf , n ) 2p -6-i s dominant.) F i n a l state interactions between the photodisin-tegration products were neglected. Furthermore, i n the treatment of helium-3, the coulomb inte r a c t i o n between the two protons was treated as a perturbation, the t r i t o n and helium-3 wave functions thus being i d e n t i c a l i n zeroth order. Of course a coulomb ba r r i e r correction must be applied to the f i n a l cross section f o r helium-3. Verde (1950) and Gunn and Irving (1951) calculated the 2 and 3-body cross sections assuming a Gaussian wave function f o r the ground state of the t r i t o n : where 1T\\: i s the distance between the i f c J l and J** 1 nucleons i n the nucleus, and JLK i s a size parameter found by equating the difference i n binding energy of t r i t i u m and helium-3, 0.76 mev, to the coulomb energy of helium-3. This form of wave function i s a n a l y t i c a l l y a t t r a c t i v e ; however, the asymptotic form f a l l s o f f f a s t e r than the correct s o l u t i o n . The f i n a l state wave function f o r 2-body breakup was taken as the product of the - 1 part of a plane wave f o r the nucleon and a pure S-state Gaussian function f o r the deuteron. That i s , y o< [ s i ^ l \u00bb - cos kr 3 ] e x p O o l J -7-where k i s the momentum of the nucleon, r 3 i s the p o s i t i o n co-ordinate of the nucleon and r l g i s the r e l a t i v e co-ordinate of the proton and neutron i n the deuteron. This c a l c u l a t i o n considers only the e l e c t r i c dipole o t r a n s i t i o n from the Sj. ground state to a continuum P-state. s Yerde shows that the magnetic dipole t r a n s i t i o n f o r the 2-body breakup i s forbidden on the basis of symmetry arguments. For 3-body breakup, the magnetic dipole t r a n s i t i o n i s not forbidden and Yerde gives an expression f o r the cross section using two plane waves f o r the f i n a l state wave functions. The cross sections for 2 and 3-body breakup are shown i n Figures 2 and 3. Gunn and I r v i n g (1951) have also evaluated the 2 and 3-body e l e c t r i c dipole photodlsintegration cross sections using ground state wave functions having a more suitable asymptotic behaviour. These wave functions are of the form This class of wave functions i s known as Ir v i n g functions. Gunn and I r v i n g evaluated (T(2-body) and ^(3-body) f o r n 5=1 1\/2 although n = 1\/4 gives the best value f o r the binding energy and coulomb energy difference f o r the 3-body system. Rossetti (1959) has evaluated (^(2-body) f o r n - 0 . In both cases the f i n a l state was assumed to be the Jt^l part of a P H O T O M E M E R G V , E t ( M E V ) Figure 2 Theoretical Estimates of the Cross Section for the Reaction He ()f , p) D (T (mb) 3 n V E R D E (,l950) ~ G A U S S I A N W A V E FUMCTIOM . - G U N N A N D I R V I N G (V9S0\" I R V L K L < \u00bb W A V E F U N C T I O N '\/yx - 2.\u20ac> F 20 25 3o P H O T O N E M E R G Y ( M E V ) FIGURE 3 'Theoretical Estimates of the Gross Section f o r the Reaction He 3(V , n) 2p - 8 -plane wave and the deuteron wave function was of the form These r e s u l t s are also given i n Figure 2. Eichmann (1963) has Improved the 2-body calculations by-considering quadrupole contributions to the cross section, by including a non-symmetrical component S' i n the ground state wave function, and by Including f i n a l state i n t e r a c t i o n s between the outgoing p a r t i c l e and the deuteron, Eichmann takes the symmetric part of the ground state wave function as a sum of two terms of the form exp \\\\-\/Az { r\\ +\u2022 r 4| + r 2|)] and chooses the parameters yj^ from a v a r i a t i o n a l c a l c u l a t i o n of the binding and coulomb energies of t r i t i u m and helium-3. The mixed symmetry state S' i s added with an amplitude r a t i o of % - O, \\ , consistent with the neutron absorption by deuterium at low energies (Austern, 1.951, 1952). The f i n a l state wave function i s taken as the product of wave functions f o r the deuteron ground state (the sum of two Gaussians) and the outgoing nucleon. The nucleon wave function Is assumed to be the Jl- 1 part of a plane wave i n one c a l c u l a t i o n . The e f f e c t of f i n a l state i n t e r a c t i o n i s calculated f o r the t r i t o n i n a second c a l c u l a t i o n , where the int e r a c t i o n i s calculated using a Serber p o t e n t i a l with a Gaussian shape. The e f f e c t s of including the mixed symmetry component, the quadrupole contribution and the f i n a l state i n t e r a c t i o n are shown i n Figure 4. The mixed symmetry component contributes to 0.9-o.e-0.7-0.6-(rr,b) 0-5-0.4-03-0.2-0.1-I.O-i 0.9-0.9-W 06-0.5-0.4-0.3-0.2-0.1-' \/ V % \/ \/ \/ \/ M e B l * , p ) D \" ^ ^ 0 \/ \/ E l (S-^P) \" ^ O ^ \/ \/ E l CS-*-P) + E 2 (S-*-D) \"^r^ \/\/ E l (.S+S'-^P) + E2 (S-t-S'-^D) 5.5 10 15 v io 25 30 PHOTON ENERGY (rAE\\l) \/ \/ I ^ _ \\ 1 S ^ N . \\ If \/ ; T ( t , n ) D N N ^ 1 El ( S - * - P ) jl \u00a3| (S -* - P) + FINAL S T A T E INTERACTIONS (o'.zto \\'o ife 20 2'S 3b PHOTOM ENERGY (MEV) FIGURE 4 He 3()T , p)D and ?(t > n)D Cross Sections from Eichmann (1963) -9-the e l e c t r i c dipole t r a n s i t i o n s (S* \u2014>\u2022 P) and lowers the energy of the cross section maximum by 10$, increasing the magnitude of the cross section by 10%. The e l e c t r i c quadrupole contribution has a dramatic e f f e c t on the > t o t a l . cross section as i s shown i n Figure 4, even for channel energies of 15 mev. The f i n a l state i n t e r a c t i o n increases the maximum cross section f o r the photodisintegration of t r i t i u m by 25% and causes the cross section curve to f a l l more r a p i d l y above the maximum. Delves (1960, 1962) has calculated the 2-body cross section f o r helium-3 at low energies and the 3-body cross section f o r t r i t i u m including the effects of f i n a l state i n t e r -actions i n the l a t t e r case. These calc u l a t i o n s are not ap p l i c -able to the present work and w i l l not be discussed here. The t h e o r e t i c a l c a l c u l a t i o n s and experimental results for the photodisintegration of helium-3 w i l l be compared i n Chapter VI. -10-CBAPTER I I I Photodisintegration of 5-body Nuclei  Experimental Results Apart from the U.B.C. r e s u l t s , there have been four experimental measurements reported on the photo-effect i n helium-3 and one on t r i t i u m . Each of these w i l l be discussed i n some d e t a i l with p a r t i c u l a r emphasis on the experimental technique. Berman et a l (1963, 1964) measured the 90\u00b0 d i f f e r e n -t i a l cross section f o r the 2-body breakup at photon energies from 8.5 to 22 mev. The experiment was done with the brems-strahlung photon beam of a 22 mev betatron incident on a helium-3 gas target. Protons and deuterons from the 2-body breakup were counted i n coincidence using two CsI(Tl) s c i n t i l -l a t o r s as detectors. Because the photon momentum i s small at these energies, the proton and deuteron are emitted at approximately 180\u00b0 to each other, with nearly equal momenta. Consequently, the energy of the proton, i s twice that of the deuteron. This constitutes a unique signature for a 2-body event and also determines the energy of the photon which caused the event. 2-body events are thus e a s i l y separated from 3-body events f o r which no such angular c o r r e l a t i o n or kinematical r e s t r i c t i o n s apply. The photon f l u x per unit energy i n t e r v a l was determined by monitoring the t o t a l energy i n the photon beam and assuming a brem^strahlung spectrum shape. -11-The r e s u l t s obtained by Berman et a l are shown i n Figure 5 and tabulated i n Table I . TABLE I 90\u00b0 D i f f e r e n t i a l Cross Section for H e 3 ( ^ ,p)D from Berman, Koester and Smith (1964) Gamma Ray Energy (mev) ( 0 ^ ) 9 0 \u00b0 steradian 9 80.0 5.0 10 90.8 5.7 11 91.6 5.9 12 88.8 6.0 13 84.5 6.1 14 78.2 5.9 15 77.1 6.5 16 6,4.8 + 6.0 17 59.9 \u00b1 5.8 18 59.7 \u00b1 6.0 19 57.6 \u00b1 6.2 20 57.5 \u00b1 6.7 21 42.7 + 6.6 .09 STeroduqn \u202206 \u202205-\\ \u2022o4-\u2022cs-\u202202.-\u202201H S T E W A R T E T A L , Y A L E B E R M A N E T A L . ILLIWOIS FlMCKH ET AL, HEIDELBERG -1\u2014\u20141 1 1 1 1 1 1 r -10 15 ~ i 1 r \u2014 r ~ 20 -< 1\u2014 25 30 G A M M A R A Y E N E R G Y (MEV) FIGURE 5 He3()T , p)D Differential Cross Section at 90\u00b0 in the Laboratory System -12-The errors quoted are c e r t a i n l y most optimistic i n view of the continuous photon energy spectrum produced by the betatron. In addition to the 2-body data, Berman et a l observed 3-body breakup i n the cases where the two protons were emitted at 90\u00b0 and 180\u00b0 to each other. Although an attempt i s made to extract a cross section for 3-body breakup from the data, the assumptions made are most l i k e l y i n c o r r e c t , and we s h a l l not reproduce the data here. Finckh et a l (1963) also measured the 90\u00b0 d i f f e r e n t i a l cross section for the 2-body breakup. Their technique was almost i d e n t i c a l to that of Berman et a l . A 31 mev bremsstrahlung beam was used to i r r a d i a t e a helium-3 gas target. The reaction products were detected by CsI(Tl) s c i n t i l l a t i o n counters. The absolute value of the cross section was determined by comparing the He ( )f ,p)D y i e l d to the known y i e l d from the reaction C 1 2 ( ) f j n J C 1 1 . In th i s manner, uncertainties i n the bremsstrahlung spectrum shape were eliminated. The re s u l t s are shown i n Figure 5. The estimated uncertainty i n the absolute value of the cross section amounts to about \u2022 1: 12%. Stewart et a l (1964) have also measured the d i f f e r -e n t i a l cross section at 90\u00b0 i n the laboratory system f o r the 2-body, breakup of helium-3. Helium-3 contained i n a c e l l was i r r a d i a t e d with, a 40 mev bremsstrahlung beam produced by an electron l i n e a r accelerator. The reaction products emitted at 90\u00b0 to the photon beam passed through a thi n window i n the c e l l and were momentum selected by a quadrupole magnet. The magnet -13-focussed the p a r t i c l e s onto two s o l i d state transmission counters arranged to stop the deuterons i n the f i r s t counter and protons i n the second counter. The energy spectrum of the photons was determined by replacing the helium-3 with deuterium and normalizing the He (^ J P)!* y i e l d to the known D()f ,p)n y i e l d . The r e s u l t s are given i n Figure 5 and tabulated i n Table I I . TABLE I I 90\u00b0 D i f f e r e n t i a l Cross Section f o r He 3(tf ,p)D from Stewart, Morrison and O'Connell (1964) Gramma Ray Energy (mev) VdJl\/90\u00b0 \/steradian 8.9 \u00b1 0.4 83 13 10.3 \u00b1 0.5 90 11 12.6 \u00b1 0.8 87 \u00b1 13 13.6 \u00b1 1.0 90 \u00b1 11 14.4 \u00b1 1.2 85 \u00b1 10 15.6 \u00b1 1.3 74 \u00b1 8 16.8 \u00b1 1.5 70 \u00b1 9 18.8 \u00b1 1.8 64 \u00b1 8 20.0 \u00b1 2.0 59 \u00b1 7 23.0 2.5 50 \u00b1 6 27.7 \u00b1 3.3 32 + 4 34.3 \u00b1 4.3 19 \u00b1 4 41.0 5.5 18 \u00b1 8 46.1 \u00b1 6.1 10 7 -14-Due to momentum considerations, the number of deuterons counted by the s i l i c o n detector should be equal to the number of protons produced i n the 2-body breakup of hellum-3. Thus any \"excess\" protons could be attributed to 3-body breakup. Stewart et a l measured the number of 3-body events as a function of proton energy and compared the i r r e s u l t s with a t h e o r e t i c a l c a l c u l a t i o n using the Irving wave function. Becchi et a l (1964) have used a 30 mev bremsstrahlung photon beam and s o l i d state p a r t i c l e detectors to measure the 90\u00b0 d i f f e r e n t i a l cross section f o r the 2-body breakup of helium-3. Their r e s u l t s suffer from poor s t a t i s t i c s and are reported i n terms of a t o t a l cross section, i n spite of the f a c t that t h i s i s not what was measured. No information i s tendered as to the method of determining the bremsstrahlung spectrum shape. Certainly, more information about the experimental technique i s required before the measurements can be taken s e r i o u s l y . The work of Gorbunov and Varfolomeev (1963, 1964) together with the U.B.C. r e s u l t s represent the only measurements of the t o t a l cross section f o r the 2 and 3-body breakup of helium-3. Gorbunov and Varfolomeev used a cloud chamber contain-ing helium-3 and a bremsstrahlung beam with a maximum energy of 170 mev. Each reaction i n the chamber was photographed and i d e n t i f i e d by i t s klnematical features. The t o t a l cross sections, 0\"(2-body) and <f (3-body), were measured and are shown i n Figure 6. The t o t a l y i e l d s f o r the two processes were found to be equal. The angular d i s t r i b u t i o n of the 2-body \\o 2o 3o 4o 50 60 70 80 9o loo G f t M M A RAY EMERGY (t^6V) FIGURE 6 Gross Sections for the Reactions He3( )f, p)D and He 3(Y , n)2p from Gorbunov and Varfolomeev (1964) -15-reactlon products was found to be I (e) = sin^e L I + (o.fc^io.io)cos\u00a9 + (o.4-fc \u00b1 o,io) cos*e] 4 ( 0 . 0 3 \u00b1 o.oi) where a l l 2-body events are included. Experimental values of the integrated cross section were obtained. The integrated cross section due to e l e c t r i c dipole absorption can be written oo (<r.L, - f^Mdiu o where LO i s the photon energy. The experimental values are < \u00a3 ( 2 - b o d y ) =\u2022 ( 2 G . 5 \u00b1 W*) rnev - n o b < \u00a3 ( 3 - b o c | y ) - ( 4 3 . < b \u00b1 2 . 7 ) r vxevz -mb The E2 contribution to (T[2-body) i s estimated to be 11 \u00b1 4%. The t o t a l cross section f o r the 2-body photodlsinte-gration of t r i t i u m has been measured by Bosch et a l (1964) using monoenergetic gamma rays from (n, tt) reactions. A tr i t i u m gas target was ir r a d i a t e d with gamma rays and the photo-neutrons were detected by a long counter. The cross section at gamma ray energies of 6.7, 7.6 and 9 mev was determined by comparing the y i e l d from the T( tt,n)D reaction with the known y i e l d from the D(tt ,p)n reaction. The assumption was made that -16-th e photoneutrons from t r i t i u m , l i k e those from deuterium, display a Sin 2\u00a9 angular d i s t r i b u t i o n . At these energies, this assumption i s v a l i d as e l e c t r i c dipole absorption w i l l dominate. The r e s u l t s are given i n Table I I I . TABLE I I I Cross Section f o r the Reaction T(tf\",n)D Gamma Ray Energy (mev) Cross Section (mb) 6.7 .075 \u00b1 .012 7.6 .295 \u00b1 .035 9.0 .57 \u00b1 .07 -17-CHAPTER IV Apparatus and Experimental Arrangement  for the Photodisintegration Measurement. A. Introduction The measurement of the t o t a l cross section f o r the reaction He 3(}f,p)D at photon energies of 8.06 and 9.17 mev i s an extension of previous work by Warren et a l (Appendix E) and Robertson (1963) who measured the cross section at photon energies of 6.14, 6.97 and 7.08 mev. A b r i e f description of the apparatus and experimental arrangement which Is described i n Robertson (1963) i s included here. B\u00bb C y l i n d r i c a l Gridded Ionization Chamber 1. Chamber Operation When charged p a r t i c l e s pass through a gas, they lose energy by i o n i z i n g the atoms of gas along t h e i r path. The 1 electron-positive ion pairs that are formed can be separated by an e l e c t r i c f i e l d and col l e c t e d by the electrodes which define the f i e l d . A knowledge of the amount of charge co l l e c t e d by the electrodes and the energy l o s t by the i o n i z i n g p a r t i c l e per ion p a i r produced i n the chamber gas leads to a measurement of the energy of the p a r t i c l e . In a pulse Ionization chamber, one electrode i s connected to the voltage supply v i a a high impedance. As the ions are moving toward, and being col l e c t e d by the -18-eleotrbde, a voltage pulse w i l l be generated whose ampli-tude i s a measure of the energy of the i o n i z i n g p a r t i c l e . Because the electron mobility i n gases i s of the order of 1000 times greater than that of heavy ions, the signal i s measured at the positive electrode. To reduce further the c o l l e c t i o n time of the charge and hence the r i s e time of the pulse, a t h i r d electrode, a screening g r i d , can be placed between the posit i v e and negative electrodes. This g r i d shields the posit i v e electrode from the induction charge pulse of the electrons u n t i l the electrons have passed, through the g r i d and eliminates the induction charge pulse of the po s i t i v e ions. Bunemann et a l (1949) discuss the e f f e c t s of such a g r i d i n a p a r a l l e l plate chamber and Robertson (1963) discusses the case of a c y l i n d r i c a l chamber. 2. Chamber Construetlon The chamber i s shown i n Figure 7 and the important dimensions are summarized i n Table IT. The c y l i n d r i c a l w a l l , A, was made of 0.25 inch thick Alcan 65ST6 aluminum tubing, turned e c c e n t r i c a l l y on a lathe to reduce the thickness to 0.050 inches on one side. The seals between the cylinder and the end plates, B, were made using Kel-F 0-rlngs. Aluminum rings, C, were used to clamp the cylinder to the end plates. F i e l d defining guard rings, E and F, were supported by insulated e l e c t r i c a l terminals. Lava discs held the g r i d supports, G. The g r i d was made of FILLING SYSTEM FIGURE 7 Ionization Chamber TABLE IT Chamber Dimensions Inside radius of cylinder wall Radius of c o l l e c t o r Mean radius of g r i d Diameter of g r i d wires Number of g r i d wires Inner guard r i n g (radius to centre of ring) Outer guard r i n g radius Distance between g r i d supports, length of active volume Inside length of chamber Approximate t o t a l volume of chamber Tota l volume i n active region between guard rings Volume of electrode support as a f r a c t i o n of V t o t Volume enclosed by g r i d as a f r a c t i o n of V. . tot Active volume Measured chamber capacity Chamber capacity and ampli f i e r input capacity Dimension 5.72 \u00b1 .05 cm 0.0507 \u00b1 .0006 cm 0.385 \u00b1 .005 cm 0.0058 cm 15 1.75 cm 3.65 cm 14.4 * .025 cm 21.5 cm 2.2 l i t e r s 1480 \u00b1 15 cc 2.20% 0.45% 1455 \u00b1 15 cc 10 \u00b1 2 pF 18 i 3 pF -19-15 strands of equally spaced s t e e l wire 0.004 i n . diameter. The c o l l e c t o r , J, made of 0,025 i n .diameter German s i l v e r tubing, was supported at one end by a Kovar sea l , M, attached to the electrode support structure and by a Kovar s e a l , P, at the other end. A glass bead, N, separated the c o l l e c t o r from i t s supporting Kovar se a l at one end, which was connected to the same voltage as the c o l l e c t o r i n order to eliminate e l e c t r i c a l noise due to tracking across the glass bead. The complete inner structure was mounted on a s~teel frame, D, and centred within the cyli n d e r . The cylinder w a l l , the end plates, and the guard rings were shielded from the p o s i t i v e electrode by a Mylar f i l m , not shown i n the di a -gram. The Mylar f i l m was e f f e c t i v e i n reducing the chamber background due to natural r a d i o a o t i v i t y i n the s t r u c t u r a l m a t e r i a l . The end of the c o l l e c t o r from which the sign a l was taken was connected to P, which i n turn was insulated from ground by another glass section, 0, Details of the sign a l end of the c o l l e c t o r are shown i n Figure 8. The electrode voltage supply i s shown i n Figure 9. A p u r i f i e r containing a Ca-Mg eutectic mixture ( C o l l i , 1952) was attached to the chamber at H* The gas was ci r c u l a t e d through the p u r i f i e r by a solenoid driven piston pump (Appendix H). The p u r i f i e r removed hydrogen, oxygen, nitrogen, carbon dioxide and water vapour impurities which were detrimental to the operation of the chamber. FIGURE 8 Details of Collector Support F COLLECTOR SUPPORT M COLLECTOR SHIELD COLLECTOR FIELD DEFINING' RINGS GRID I M N E R I OUTER \u2014 \u2014 - 0 0 7 5 y * F |o M51 w v w 10 M i l v V W V TEST PULSE INPUT 10 MSI 50 pF CASCODE INPUT STAGE OF DYNATRON PREMA9L\\F\\ER 2 p F E.H.T SUPPLY 0 TO 5.5 KV I X T FIGURE 9 Electrode Voltage Supply J _ 6 K V DCWV 2.5 M51 .02 \/ 4 2 MSI :02\/ < F FIELD DEFINING R\\NG VOLTAGES V 0 = O . \\GG \\\/GRvD -20-3. Gas Mixtures The gas mixtures used in the chamber had to satisfy three criteria. a) The gas mixture had to be dense enough so that the reaction particle ranges were appreciably shorter than the diameter of the chamber. If this were not so, a l l the particles produced in the reaction would lose a portion of their energy in collision with the wall and consequently the voltage pulse height would not be indicative of the energy of the particle. The ranges of protons and deuterons in various gases are shown in Figure 10. It is obvious that helium-3 alone would not suffice to stop the reaction products which have energies of from 1 to 2 mev. For this reason, argon, a gas with a higher stopping power, was added. For such a mixture of gases, the range, R^ *^ is approximately given by where P^ , Pg...are the partial pressures of the gases in atmospheres and R^ , R2,...are the ranges in the gases at N.T.P. b) The gamma flux produces a large flux of electrons through the chamber. These electrons are a result of Compton, pair production, and photoelectric interactions between the photons and the material FIGURE 10 Charged Particle Ranges in Gases at 15\u00b0 C and 76 cm Pressure. From Whaling (1956) -21-surrounding the chamber and the gas contained In the chamber. Because of the low stopping cross section of the electrons compared to heavy oharged p a r t i c l e s , these electrons lose r e l a t i v e l y l i t t l e of t h e i r energy within the active volume of the chamber. However, i f many electrons traverse the chamber within the resolving time of the electronics, large voltage pulses can occur due to the pile-up of small pulses. I t i s therefore important to keep both the r i s e and f a l l times of the pulses as small as possible. To reduce the c o l l e c t i o n time and the resolving time of the apparatus, methane was added to the argon and helium-3 . For a given c o l l e c t o r voltage and gas pressure the methane reduced the r i s e time of the pulses by a factor of two. The requirements of a high stopping power fo r heavy charged p a r t i c l e s and a low stopping power fo r electrons cannot be simultaneously s a t i s f i e d . However, with the f a s t e r r i s e times achieved with the addition of methane, the increase of electron noise with higher gas pressures could be tolerated. e) The gas mixture chosen had to produce s a t i s f a c t o r y energy re s o l u t i o n . This c r i t e r i o n set a lower l i m i t of 3.2 microseconds on the amplifier d i f f e r -e n t i a t i o n time constant and an upper l i m i t on the t o t a l pressure i n the chamber. -22-The t o t a l amount of gas which could be contained i n the chamber was l i m i t e d by two fa c t o r s . F i r s t , the thin w a l l of the chamber could only withstand pressures up to 10 atmospheres, an obvious upper l i m i t on the t o t a l pressure. However, at these high pressures, the ion density along an i o n i z a t i o n track becomes so great that recombination of the electron-positive ion pairs may take place. In a uniform e l e c t r i c f i e l d t h i s e f f e c t r e s u l t s i n a lower pulse height f o r a fixed energy i o n i z i n g p a r t i c l e . In a non-uniform f i e l d , such as that which ex i s t s i n a c y l i n d r i c a l chamber, the recombination eff e c t i s greater i n low f i e l d regions near the w a l l with a r e s u l t i n g spread i n pulse heights, and a subsequently poorer energy res o l u t i o n . The amount of recombination which takes place i s a function of the s p e c i f i c i o n i z a t i o n of the i o n i z i n g p a r t i c l e , the mixture of gases i n the chamber and the r a t i o of the e l e c t r i c f i e l d to t o t a l gas pressure. In order to keep the recom-bination to a minimum for the proton and deuteron tracks i n the chamber, the t o t a l pressure was l i m i t e d to a value of 8 atmospheres. Consideration of the foregoing c r i t e r i a led to the chamber f i l l i n g s given i n Table V. -23-TABLE V Chamber f i l l i n g s . Gas pressures i n Atmospheres at 0\u00b0C Helium-3 Methane Argon 8.06 mev run 2.24 0.218 5.32 9.17 mev run (2-body 1.515 0.251 5.08 breakup) 9.17 mev run (3-body 1.41 0.19 1.36 breakup) C. Energy C a l i b r a t i o n of the Chamber The rate of energy loss from a charged p a r t i c l e i n a gaseous media has three components, one due to i o n i z a t i o n , one due to e x c i t a t i o n and one due to e l a s t i c i n t e r a c t i o n . The t o t a l rate of energy loss i s given by d* ax dx u cU where n^, n m and nq ref e r respectively to i o n i z i n g , e x c i t i n g and e l a s t i c c o l l i s i o n s with energy c o e f f i c i e n t s i , m and q.. The average energy l o s t by the charged p a r t i c l e through a l l processes per ion pair formed i s - 2 4 -For a given gas or mixture of gases,W i s nearly independent of the nature of the charged p a r t i c l e or i t s v e l o c i t y . However, values of w vary considerably f o r d i f f e r e n t gases or mixtures of gases. The i n c l u s i o n i n a gas of a contaminant able to destroy metastable states by an i o n i z i n g c o l l i s i o n (for example, argon i n neon) w i l l increase n^ at the expense of n m and thus decrease the value of w. For a given value of w and a given number of ion p a i r s , the voltage pulse height i s determined by the f r a c t i o n of the electrons which are ultimately c o l l e c t e d . When a l l the electrons are c o l l e c t e d , saturation has been achieved. In general, two processes i n h i b i t complete c o l l e c t i o n . I f electronegative atoms or molecules are present i n the i o n i z a t i o n chamber, electrons may attach to them and the heavy negative ion thus formed migrates slowly toward the c o l l e c t o r and i s removed from the f a s t component of the voltage pulse. For a given gas, the p r o b a b i l i t y of electron attachment depends on the energy with which the electron s t r i k e s the electronegative atom or molecule. Roughly speaking, this p r o b a b i l i t y i s decreased as the electron v e l o c i t y increases; that i s , as the e l e c t r i c f i e l d increases, or the gas pressure decreases. Figure 11 shows a graph of voltage pulse height C I A versus c o l l e c t o r voltage f o r 5.3 mev alpha p a r t i c l e s from P Q . Curve \"A\" was taken from data before the mixture was p u r i f i e d , hence with a probable admixture of electronegative gases. Curve \"B\" i s taken from data a f t e r p u r i f i c a t i o n and indicates that saturation i s much more complete. A O Q B E F O R E P U R \\ F V I ^ G _ -looo 2ooo 3ooo 4ooo COLLECTOR VOLTAGE (VOLTS) FIGURE 11 Effect of Purification on Voltage Pulse Amplitude -25-The second process which i n h i b i t s complete c o l l e c t i o n i s columnar recombination of electrons and positi v e ions along an i o n i z a t i o n track. The amount of recombination i s a function of the density of ion p a i r s along the track and the magnitude of the e l e c t r i c f i e l d . For a given f i e l d , the ion density depends on the t o t a l pressure and on the s p e c i f i c i o n i z a t i o n of the charged p a r t i c l e . Since the s p e c i f i c i o n i z a t i o n i s di f f e r e n t for protons, deuterons and alpha p a r t i c l e s , i t i s possible to achieve complete c o l l e c t i o n f o r proton and deuteron tracks while having incomplete c o l l e c t i o n f o r alpha p a r t i c l e tracks. Such an e f f e c t has been observed i n the chamber used i n t h i s experiment. The Q-value fo r the photodisintegration of argon-40 into an alpha p a r t i c l e and a sulphur-36 nucleus Is -6.764 mev. This reaction has been observed at U.B.C, (Appendix 3\"), at a gamma ray energy of 9.17 mev. The argon was placed i n a gridded c y l i n d r i c a l i o n i z a t i o n chamber and irr a d i a t e d with gamma rays from the proton bombardment of car-bon-13 (Appendix C). The known energy of the alpha p a r t i c l e s , 2.41 mev, agreed very w e l l with the energy of the alpha group i n the speotrum as established i n terms of a plutonium 239, 5,15 mev alpha souroe. Because : pure argon was used, complete c o l l e c t i o n of the electrons was achieved at usable values of c o l l e c t o r voltage. As Robertson (1963) shows, the addition of methane and\/or helium to argon increases the co l l e o t o r voltage required to achieve saturation. For the gas mixtures used i n -26-the helium-3 experiment, oomplete c o l l e c t i o n f o r the alpha p a r t i c l e s was not achieved. Because argon was used as a stopping gas i n the chamber, the photoalphas from argon were observed during the photodisintegration of helium-3 experiment. The energy of the alpha group was predicted c o r r e c t l y by the 5.3 mev P o 2 1 0 c a l i b r a t i o n source over a wide range of gas pressures. However, the energy of the proton-deuteron group from the photodisinte-gration of helium-3 was not predicted c o r r e c t l y at a l l pressures. The agreement was reasonable, though not exact, f o r the low pressure runs of Warren et a l , whereas at the pressures used i n the present experiment the 3.67 mev photodisintegration group was found at an energy which would be interpreted as 210 being 5.0 mev as predicted by the P 0 c a l i b r a t i o n source i n the chamber. Although saturation i s not achieved at high pressures f o r the alpha tracks, saturation i s much more complete f o r the proton-deuteron tracks. That i s , a greater percentage of electrons i s c o l l e c t e d . At lower pressures, c o l l e c t i o n i s more complete f o r the alpha tracks and consequently the agree-ment i n the energy scale between the alpha p a r t i c l e s and the protons and deuterons i s better. When c o l l e c t i o n i n the chamber i s not complete, a given voltage pulse height corresponds to d i f f e r e n t energies, depend-ing upon whether the i o n i z i n g p a r t i o l e was an alpha p a r t i c l e or a proton. For t h i s reason, the energy scale f o r the photodis-inte g r a t i o n of helium-3 was determined using .the reaction -27-He (n,p)T. The voltage pulse amplitude from a pulse generator (Robertson, 1957) was calibrated i n terms of the thermal neutron capture peak at 0.765 mev. The pulse generator was then used to determine the energy scale f o r each run. A further check was provided by I r r a d i a t i n g the chamber with 7.12 mev gamma rays from the proton bombardment of fluorine-19. The p o s i t i o n of the thermal neutron peak, the 7.12 photodisintegration peak and the 9.17 mev photodisintegration peak are shown i n Figure 12. The energy scale i s l i n e a r over a wide range of energies. The p o s i t i o n of the 5.3 mev o< peak i s also shown and the disagree-ment i n the two energy scales i s obvious. D. Chamber Background One of the problems associated with a low count rate experiment such as the photodisintegration of helium-3 i s that of background. I f the time taken to accumulate s u f f i c i e n t photodisintegration data i s long, a considerable number of counts w i l l be contributed to the spectrum by the natural alpha a c t i v i t y from the impurities i n commercially available materials. Table VI, taken from Sharp (1955), l i s t s the alpha p a r t i c l e backgrounds from various materials. For the work of Warren et a l , the i n t e r i o r of the chamber was coated with an aqueous dispersion of graphite known as aquadag. The background i n the chamber of t o t a l area 1000 cm3 compared favourably with the figure l i s t e d i n Table VI. Furthermore, the majority of counts were i n the region of 4 to 6 ENERGY SCALE FOR PROTONS AND DEUTERONS (wev) FIGURE 12 Chamber Energy Calibration -28-TABLE VI Alpha P a r t i c l e Backgrounds M a t e r i a l p Alphas per cm per hour of energy greater than 250 kev Machined Copper 0.09 Commercial Brass 0.05 M i l d Steel 0.03 Commercial Aluminum 0.31 Solder 28 Aquadag (Graphite) 0.07 Lead 60 A i r from room 2 32 per 100 cm per hour Cylinder argon 0 mev, well above the energy of the photodisintegration products and background was no problem. For the higher energy photo-di s i n t e g r a t i o n measurements, the energy region from 4 to 6 mev f o r alpha p a r t i c l e s corresponded to a proton-deuteron energy of from 2.7 to 4 mev. As the photodisintegration products have an energy of 3.67 mev f o r 9.17 mev gamma rays, i t was necessary to reduce the chamber background considerably. The technique which eventually proved s a t i s f a c t o r y ?\/as to l i n e the chamber with a polyester f i l m produced by du Pont under the trade name \"Mylar\". This i s a tough, transparent -29-material with a low vapour pressure, composed of 62.5% carbon, 4.2% hydrogen and 33.3% oxygen by weight. A thickness of \u20143 ? 3.6(10) cm or 5 mg\/cnr was found s u f f i c i e n t to stop a 7 mev alpha p a r t i c l e . The Mylar was coated with a thin f i l m of gold, evaporated on both surfaoes, to render the Mylar conducting. This was necessary so that the Mylar did not accumulate charge and d i s t o r t the f i e l d within the chamber. The success of this technique i s i l l u s t r a t e d i n Figure 13 which shows the e f f e c t of i n s e r t i n g the Mylar f i l m . The background with the Mylar was 0.02 alphas per cm2 per hour, uniformly d i s t r i b u t e d over an energy range from 0 to 7 mev. E. Pulse Amplification and Analysis The voltage pulses appearing at the c o l l e c t o r of the chamber were amplified by a Dynatron Preamplifier Unit and a Dynatron Main Amplifier Type 1430A. This amplification system provided a wide range of integration and d i f f e r e n t i a t i o n time constants f o r pulse shaping. The pulse shape was chosen to provide optimum energy resolution while keeping the pulse width as short as possible to reduce electron pile-up. The integra-t i o n time constant was set at 8.0 microseconds and the d i f f e r e n t i a t i o n time constant at 3.2 microseconds f o r a l l of the experimental data. The pulses from the main amplifier were fed to a Nuclear Data Model ND103, 256 channel pulse height analyzer f o r analysis and storage. The time taken f o r the kicksorter (pulse height analyzer) to record each pulse i s ('25+ ) microseconds NUMBER OF COUNTS (ARBITRARY SCALE\") H U . 1 1 I I I I 1 I I L_ -30-where N i s the channel i n which the pulse Is stored. The t o t a l time during which fche analyzer w i l l not accept a pulse i s referred to as \"dead time\". I f the dead time i s an appreciable f r a c t i o n of the t o t a l time of the run, a correction must be made to account for those pulses which were not analyzed. The kicksorter records the dead time so that the true number of pulses N which appeared at the kicksorter input i s given by N - -I-N' T - t where T i s the t o t a l time of the run, t i s the dead time and N' i s the number of pulses accepted by the k i c k s o r t e r . During this experiment, the dead time never exceeded 2% of the t o t a l time. F \u00bb G^ mma Flux Measurement The integrated gamma f l u x was measured with a 2\u00a7 inch diameter by 4^ inch long Nal(Tl) s c i n t i l l a t i o n counter. The measurement of the e f f i c i e n c y f o r this c r y s t a l i s described i n Appendix C. The output of the photomultiplier was fed through a cathode follower to a Nuclear Data Dual Amplifier Model ND501. This a m p l i f i e r also served as a single channel analyzer. The discriminators of the single channel analyzer were set so that St-all pulses corresponding to -ry mev energy release i n the c r y s t a l were fed to a Model U.B.C.-NP-ll scalar and counted. Pulses from a pulse generator (Robertson, 1957), fed Into the cathode -31-follower of the counter, were used to set the discriminators. The pulse generator voltage l e v e l was calibrated i n terms of gamma ray energy release i n the c r y s t a l by using the f u l l energy peak i n the 2.62 mev gamma ray spectrum of a Ra Th source. The gamma ray speotrum was continuously recorded by feeding the output of the ND501 amplif i e r into a Nuclear Data Model ND 120, 512 ohannel pulse height analyzer. In thi s manner, a constant cheok was maintained on the bias l e v e l , and the speotrum shape was continuously monitored. Typical gamma spectra are shown i n Appendix C. The c a l c u l a t i o n of the gamma flux through the chambers i n terms of the gamma f l u x recorded by the s o l n t i l l a t l o n counter i s discussed i n Appendix A. G. Experimental Arrangement The experimental arrangement i s shown i n Figure 14. The target and Ionization chamber were surrounded by a castle of wax and cadmium to sh i e l d the chamber from neutrons. The castle wall consisted of 6 inches of wax and 0.15 inch thick cadmium sheathing. The only dlreot path into the castle was the I f inoh diameter hole f o r the beam tube. The chamber was supported In an adjustable rack whioh sat on the bottom of the c a s t l e . The carbon-13 targets were prepared by thermally crack-ing methyl iodide onto .002 Inch thick platinum backings. The technique i s discussed i n Appendix B, The platinum target W A T E R C O O L I N G I O N I Z A T I O N . C H A M B E R WAX C A D M I U M C O L D TRAP -5 P R O T O N B E A M F R O M V A N D E GRAAFF P Y R E X B E A M T U B E ^777 \/\/\/' \/ \/ \/ \/ ^ \/ \u2014 V\"\/\/' TAvRGET FIGURE 14 Experimental Arrangement -32-backing was soldered with indium onto the target support which consisted of a loop of 3\/16 inch copper tubing. The target was cooled by passing water through the copper tubing,and beam currents up to 30 microamps produced no deterioration of the target. The s c i n t i l l a t i o n counter was placed outside the castle wall i n a po s i t i o n such that the only material between the counter and target was the castle wall i t s e l f . The percentage of gamma rays absorbed i n the castle wall was determined by measuring the difference i n gamma flux per microcoulomb of proton current with and without the.oastle. The measured trans-mission factors f o r 8.06 and 9.17 mev gamma rays agreed with those estimated from the gamma ray attenuation c o e f f i c i e n t s f o r p a r a f f i n and cadmium. -33-CHAPTER V Photodisintegration Results and Estimation  of the Cross Section at 8.06 and 9.17 mev A. Spectrum at 8.06 mev The spectrum obtained f o r the reaction He ,p)D at a gamma ray energy of 8.06 mev i s shown i n Figure 15. The deter-mination of the energy scale i s discussed i n Chapter IY. The background shown i n Figure 15 and used i n the cross section analysis was e n t i r e l y due to res i d u a l r a d i o a c t i v i t y i n the walls of the chamber. When the helium-3 i n the chamber was replaced by helium-4, the spectrum i n the region of Interest was the same, with and without a gamma f l u x present. This was the case f o r both 8.06 and 9.17 mev gamma rays and j u s t i f i e s the use of the time dependent (gamma ray independent) background i n the 2-body breakup cross section analysis. B. Spectrum at 9.17 mev - 2 rbpdy Breakup A t y p i c a l spectrum obtained at a gamma ray energy of 9.17 mev i s shown i n Figure 16. The energy scale applies only to the photodisintegration of helium-3 as discussed i n Chapter IY\u00ab The background i s again due to r e s i d u a l r a d i o a c t i v i t y i n the chamber and i s much lower than for the 8.06 mev run because of the effectiveness of the Mylar shi e l d (see Chapter IY), which was inserted a f t e r the 8.06 mev run was completed. 2oo-\u00bb8o-I60-!4o-h z 120-D O U loo-U- 8o-o or 6o-IU CO 40-Z 20-r o 4-3 4 3 2-j io H 6 4-~~r~ o \u00a9 \u00a9 PHOTODIS INTEGRAT ION SPECTRUM \u2022 \u2022 T I M E D E P E N D E N T B A C K G R O U N D x x R a - Be N E U T R O N SOURCE <g) E L E C T R O N P ILE-UP S P E C T R U M O N L O G S C A L E C H A M B E R F I L L I N G IN A T M O S P H E R E S Me 3 -C H 4 . \" A R G O N -to \u2014r 2o 1 \u2014 30 K I C K S O R T E R 1 1\u2014 4-0 50 C H A N N E L \"io\" 1 70 T z E N E R G Y ( M E V ) 3 -1 4-( P R E S S U R E S A T 0\u00b0C) 2 . 2 4 -0 . 2 1 8 5 . 3 2 FIGURE 15 Photodisintegration Spectrum, 8.06 mev Gamma Rays -O PHOTO DISINTEGRATION! SPECTRUM IOO-9o 8 0 -70-<oO-50-40-30-2o-lo-r o l i k \\ \\ \\ \\ T \u2022 T I M E D E P E N D E N T B A C K G R O U N D X X Ra-Be N E . U T R O M S O U R C E ^ \u00ab L , T I O O 6 I I T T 1 VO 20 30 K lCXSORTER T 4rO 50 C H K N N I E L , \u2014 I \u2014 6 o 2 T 3 ENERGY (MEV) T\" 4-CMAhABER FILLING (PRESSURES ATMOSPHERES AT O \u00b0 C) H e 3 - 1.515 CH4. \"\" 0-^5 \\ A R G o N ~ S . 0 8 \u2014r\u2014 TO 80 FIGURE 16 Photodisintegration Spectrum for the Reaction He 3 ( Y , p)D at a Gamma Ray Energy of 9.17 mev -34-C. Speotrum at 9.17 mev - 5-body Breakup The 2-body photodisintegration data was obtained with a t o t a l gas pressure of 6.846 atmospheres (at 0\u00b0C). The high pressure was required to reduce the wall loss to a reasonable value. As a r e s u l t of this high gas density, the gamma ray induced electron spectrum extended to 2 mev. The 3-body breakup spectrum, which extends from 0.49 to 1.47 mev, was thus t o t a l l y obscured by the electron noise. In order to see the 3-body spectrum, the t o t a l gas pressure was reduced to 2.96 atmospheres. Figure 17 shows the 3-body spectrum obtained f o r the chamber f i l l i n g indicated. The electron end point has been reduced to 0.57 mev as a resul t of the lower t o t a l pressure and because the gamma f l u x was decreased to reduce pile-up. The dominant contribution to the background i n the region of the photodisintegration spectrum was due to neutron induced disintegrations (Appendix D). The background shown i n Figure 17 was obtained with the proton beam on the carbon-13 target but o f f resonance, so that the 9.17 mev gamma f l u x was n e g l i g i b l e . As the neutron induced back-ground was c r i t i c a l l y dependent on the proton beam energy, h a l f the background was run 12 kev above the resonance at 1.75 mev and the other half at 12 kev below resonance. Events from the 2-body breakup of helium-3 can also be seen i n Figure 17. However, the wall loss f o r the chamber f i l l i n g used was 76% so there i s no well-defined f u l l energy peak i n the spectrum. As a consequence of the lower gas pressure, the photo-alpha group from argon-40 can also be seen 50-4 o -I-? 30 o 20-o -o PHOTOOIS I N T E G R A T \\ O N S P E C T R U M + 25 _ . BEA\\M DEPENDENT BMIKGROUND C H A M B E R FILLING ( P R E S S U R E S IN A T M O S P H E R E S A T 0 \u00b0 C ) He* - 1.4-1 CH4. - 0.19 A R G O N - \\\u00abB6 H e 3 ( Y , p ) D - 1 \u2014 10 \u2014 1 1 1\u2014\u00ab 20 30 40 KlCKSORTER ^ - - \u2014(5 *~ \u2014 \u2022 - - \u2022* - \u2014 50 C H K N N E L Go 70 So 9o T \"T~ 2. T ENERGY (MEV) FIGURE 17 Photodisintegration Spectrum for the Reactions He3()f , n)2p and A 4 0 (ft ,cx) S 3 6 at a Gamma Ray Energy of 9.17 mev -35-at an energy c o r r e c t l y predicted by the thermal neutron capture peak (see Chapter IY). D \u00ab Analysis of the 2-body Data The data f o r the 8.06 and 9.17 mev runs i s summarized i n Table VII. The gamma f l u x was calculated as shown i n Appen-dix C , and correction was made f o r absorption In the wax and cadmium shi e l d where applicable. Run 2 at 9.17 mev was made without the shield i n place. The absorption i n the aluminum chamber wa l l was calculated to be 1% i n a l l cases. The photodisintegration spectra show a f u l l energy peak at E 0 = (Ey. - 5.493) mev and a low energy t a i l . This low energy t a i l i s due to those events i n which one of the reaction products s t r i k e s the wall or passes into the end region of the chamber. This e f f e c t i s termed \"wall l o s s \" and i s a function of the size and shape of the chamber and the range of the reaction products. The t o t a l y i e l d i s the sum of the number of counts In the f u l l energy peak and the number of counts i n the wal l loss t a i l . The method of determining the t o t a l y i e l d i s explained i n d e t a i l i n Appendix A. B r i e f l y , the t o t a l y i e l d i s equal to the number of counts above an energy 2E Q\/3 plus a calculated wall loss correction for those counts i n the energy i n t e r v a l from E 0\/3 to 2E 0\/3. Table VII shows the two contributions to the t o t a l y i e l d . A correction to the t o t a l y i e l d due to the \"dead time\" of the kicksorter i s explained i n Chapter IV. TABLE VII Data from Photodisintegration Spectra for He3(t , p)D 8.06 mev 9.17 mev Run 1+ Run 2 Time (hours) 8.606 3.889 5.617 Proton beam current (microamps) 16 25 23 Proton Energy (mev) 0.730 1.760 1.760 Total number of 8.06 or 9.17 mev gamma rays from target. (Includes correction for absorption in castle wall) 9 . 1 9 ( 1 0 ) 9 5 .32(10) 9 10 .87 (10 ) 9 Total number of counts from energy ^^ <j^ to EQ + &E E 0 = Ey - Q , SE = half width of peak 938 427 512 Time dependent background in energy interval ^  to EQ + SE 543 78 93 Number of photodisintegrations in i n t e r v a l t o EQ + SE * 397 . 356 421 True number of photodisintegrations in peak, Np 360 267 309 Partial wall loss correction 25 33 38 Total yield 422 389 459 *Includes correction for \"dead time\" of the kicksorter + Spectrum shown in Figure 16 -36-E. Gross Section Calculation .\u00a3&\u00a3 th\u00a3 Reaction Heg(r .n)D It is shown in Appendix A that the cross section (f is given in terms of the total yield by H(d)\/p&\\.S where H(d) is the effective path length-solid angle product for a source a perpendicular distance d from the chamber wall, is the atom density of helium-3 in the chamber, and Ny. is the total number of gammas emitted by the source. The cross section values are given in Table VIII together with experimentally measured values of d, pW g and ~&, The errors quoted are the total errors in each measured value. All the U.B.C. 2-body photodisintegration data is shown in Figure 18. The 90\u00b0 differential oross section measure-ments of Berman et al (1963) and Stewart et al (1964) are shown for comparison. At these energies, the photodisintegration is predominantly due to electric dipole absorption -with a resulting sin 6 angular distribution of the reaction products. Hence, the differential cross sections have been transformed to total cross sections by multiplying by 8 T T\/3. The results of BSsoh et al (1964) for the photodisintegration of tritium are plotted as a function of the energy of the reaction produots above the threshold energy. F. Errors in the 2-body Cross Seotion The estimated probable errors, excluding the statisti-cal variation in the number of counts observed, are summarized in Table IX. The error in determining the scintillation counter CV3H 0.74 0.6A (mb) 0.54 0.4-03 0.2' 0.1 1 T H R E S H O L D 0 T * \u00a9J. A T 0 A \u00a9 U . B . C . D A T A \u2022 B E R M A N E T A L ^ S T E W A R T E T A L V B O S C H E T A L ' T ( Y ; n)[ ENERGY A B O V E T H R E S H O L D ( M E V ) 2 3 4 - 5 , i , i . i . u_ 7 Q 9 10 P H O T O N ENERGY ( M E V ) F O R H e H t f ^ D FIGURE 18 Cross Sections for the Reactions He (V , p)D and T(tf , n)D TABLE VIII H e 3 ( \u00a3 , p)D Cross Section Data Run Yield ( from Table VII) d ( cm ) H(d) (cm-sterad.) PH. (atoms\/cm )^ V 4n cr (mb) 8.06 mev 422 + 31 2.79 \u00b1 0.1 19.7 \u00b1 0 . 5 (6.02 \u00b1 0.08)(10) 1 9 (7.22 \u00b1 0.74)(10) 8 0.493 \u00b1 0.066 9.17 mev Run 1 389 \u00b1 21 0.95 \u00b1 0.1 34.9 \u00b1 2.0 (4.07 \u00b1 0.07)(10) 1 9 (4.17 \u00b1 0.43)(10)8 0.658 \u00b1 0.089 9.17 mev Run 2 459 \u00b1 24 3.91 \u00b1 0.1 18 .29\u00b1 0.2 (4.07 \u00b1 0.07)(10) 1 9 (8.53 \u00b1 0.88)(10) 8 0.723 \u00b1 0.087 *Includes correction for absorption in chamber wall. TABLE IS Estimate of Errors 1. Error i n determining gamma f l u x at the s c i n t i l l a t i o n counter a. A f f e c t i n g each run Counter s o l i d angle \"\u00b1.1.5% Setting bias point \u00b1 0.5% b. A f f e c t i n g 8.06 mev and Run 1, 9.17 mev Attenuation i n p a r a f f i n and cadmium s h i e l d \u00b1 2% Total \u00b1 2.6% c. Systematic error i n s c i n t i l l a t i o n counter e f f i c i e n c y \u00b1 10% Tota l error i n gamma f l u x at the s c i n t i l l a t i o n counter \u00b1 10.3% 2. Error i n determining gamma f l u x through the io n i z a t i o n chamber a. Due to uncertainty of the angular d i s t r i b u t i o n of 9.17 mev gamma rays \u00b1 2.8% b. Due to uncertainty of r e l a t i v e i n t e n s i t y of 8.06 and 9.17 mev \u00b1 1% gamma rays Total \u00b1 3.0% 3. E r r o r i n H(d) due to measurement of d 8.06 mev \u00b1 2.5% 9.17 mev, Run 1 \u00b1 5.7% 9.17 mev, Run 2 \u00b1 1.1% 4 . Error i n p ' H e 8.06 mev \u00b1 1.3% 9.17 mev \u00b1 1.7% 5. Error i n y i e l d due to uncertainty of wall l o s s correction \u00b1 1% -37-s o l i d angle i s caused by inaccuracies i n the measurement of the counter area and the target,to counter distance. The error i n determining the gamma f l u x through the i o n i z a t i o n chamber i s considered i n Appendix C. The seemingly large uncertainty i n i s explained i n Appendix A. The errors f o r each run, including s t a t i s t i c a l errors i n the y i e l d measurement, are given i n Table X. The error Is calculated by adding the i n d i v i d u a l errors i n quadrature. In each case the systematic error i n the s c i n t i l l a t i o n counter e f f i c i e n c y dominates the t o t a l error. \u2022 TABLE X Cross Section Errors Run Probable Error Neglecting the Uncertainty i n S c i n t i l -l a t i o n Counter E f f i c i e n c y Total Probable Error 8.06 mev 9,17 mev-Run 1 9.17 mev-Run 2 \u00b1 8.4% \u00b1 9.0% \u00b1 6.5% \u00b1 13.3% \u00b1 13.5% \u00b1 12.0% The errors i n the absorption of the gamma rays by the chamber wa l l and the error i n assuming this absorption to be constant over the surface of the chamber are n e g l i g i b l e . The -38-absorption of the gamma rays by the glass wall of the beam tube i s assumed to be the same f o r the s c i n t i l l a t i o n counter and the chamber. The error i n thi s assumption i s l e s s than 0.4%. The error i n assuming a point source of gamma rays rather than a dist r i b u t e d source i s also l e s s than 1%. G. Estimation of the He ( ,n)2p Cross Section Using the data i n the spectrum shown i n Figure 17, a preliminary value f o r cf (3-body) can be obtained. .Unfortunately the thermal neutron capture peak from the reaction He^(n,p)T completely obscures the 3-body spectrum from 0.49 to 1.0 mev. Furthermore the wall l o s s and end e f f e c t f o r the 2-body events (Appendix A) give a s i g n i f i c a n t contribution to the t o t a l y i e l d i n the region from 1.0 to 1.5 mev. Table XI summarizes the data f o r the 3-body photo-di s i n t e g r a t i o n run. I f one assumes that the spectrum shape i s given by Figure 1, (that i s , that there are no f i n a l ,state i n t e r a c t i o n s ) , the cross section calculated from the data i s <T ( He \u2014 * ~ ^ + 2 p ) = ( 0 . 2 5 \u00b1 0.13) m b The uncertainty quoted includes a \u00b1 50% error due to s t a t i s t i c a l f l u c t u a t i o n s i n the t o t a l number of counts and 10% contributions due to uncertainties i n gamma f l u x and background subtraction. TABLE XI Data f o r 3-body Cross Section at 9.17 mev Gamma Ray Source: C 1 3 ( p , ^ ) N 1 4 at 1.75 mev resonance Time \u00a3.091 hours Proton beam current 15 mlcroamps Total number of 9.17 mev R gamma rays, Ny * 1,72(10) 4n 3-body photodisintegration data from Figure 17 Total counts 1.0 to 1.7 mev 99 Backgrounds: Beam dependent, neutron induced 29 2-body w a l l e f f e c t 36 2-body end eff e c t 14 Net number of counts from 1.0 to 1.7 mev 20 Data f o r cross section c a l c u l a t i o n 3.79(10) 1 9 H(d), d = 2.5 cm 24.5 cm-steradians 3-body wa l l loss < 10%, neglected * Includes correction f o r attenuation i n castle w a l l . -39-C H A P T E R VI Discussion of Experimental Measurements  and Theoretical Calculations on the  5-Hueleon System A. Photodisintegration of Helium-5 The t o t a l cross section measurements f o r the reaction He (}T,p)D reported i n this thesis and by Warren et a l (1963) are not Inconsistent with the measurements of Gorbunov and Varfolomeev (1964). Direct comparison of these t o t a l cross section measurements with the 90\u00b0 d i f f e r e n t i a l cross section data of Berman et a l (1963, 1964), Stewart et a l (1964) and Finckh et a l (1963) cannot be made without knowledge of the angular d i s t r i b u t i o n , o f the reaction products as a function of photon energy. Gorbunov and Varfolomeev (1964) have measured the angular d i s t r i b u t i o n but report only the angular d i s t r i b u -t i o n f o r a l l 2-body events summed over photon energies from 5,5 to 170 mev. This angular d i s t r i b u t i o n i s shown as curve A of Figure 19. Eichmann (1963) has calculated the angular d i s t r i b u -t i o n at a photon energy of 19.5 mev, with and without an e l e c t r i c quadrupole contribution to the dominant e l e c t r i c dipole absorption. For pure e l e c t r i c dipole absorption the angular d i s t r i b u t i o n I ( Q ) i s equal to s i n 2 \u00a9 . The e f f e c t of the e l e c t r i c quadrupole contribution i s shown as curve B of Figure 19, where the curve has been normalized to the same peak height R E L A T I V E Y I ELD MEASURED A*J<iULAR D \u00bb S T R \\ ^ 0 T \\ O N FoR PHOTONl ENER6\\ES> F R O M S . 5 T O \\ T O M G V . F-Rot-A G O R ^ U M O V A M D V A R F O L O M E E V (V9\u20ac>4-) C A L C U L A T E D A N G U L A R D \\ S T R \\ F C U T I O N A T A P H O T O N E N E R S Y O C 1 9 . 5 M \u00a3 V \/ F O R C L E C T R V C D I P O L E . A N D E L E C T R I C Q U A D R U P O L E A ^ S O R R T I O N . F R O M E ICr tMA^IN (V9631) 0 C M FIGURE 19 Angular Distribution of the Reaction Products for the Reaction He (ft , p)D -40-a s t h e r e s u l t s of Gorbunov and Varfolomeev. The assumption can be made that the angular d i s t r i b u -t i o n at photon energies riear 20 mev i s approximated by curve A of Figure 19. This assumption Is p a r t i a l l y j u s t i f i e d by the calculated e f f e c t of the e l e c t r i c quadrupole contribution on the d i f f e r e n t i a l cross section. In t h i s case the t o t a l cross section, <f (2-body), i s given i n terms of the 90\u00b0 d i f f e r e n t i a l cross section by Eq 6-1 where I ( \u00a9 ) i s given by Eq 6.-2 I ( \u00a9 ) i s suitably normalized so that 4\/n steradians From equations 6-1 and 6-2 we have -41-Figure EO shows the t o t a l cross section data and an average of the 90\u00b0 d i f f e r e n t i a l cross section data transformed by equation 6-3 to a t o t a l cross section. Figure 20 indicates that the t o t a l and 90\u00b0 d i f f e r e n t i a l cross sections are i n poor agreement and are inconsistent with the angular d i s t r i b u t i o n given by equation 6-2. I t i s thus u n l i k e l y that both sets of data are correct. Consideration of the experimental techniques favour acceptance of the work of Stewart et a l (1964) and Finkh et a l (1963) over the measurements of Gorbunov and Varfolomeev (1964). In the region of the cross section maximum (Egv= 10 to 12 mev), e l e c t r i c quadrupole absorption i s almost c e r t a i n l y n e g l i g i b l e and the r e s u l t i n g angular d i s t r i b u t i o n i s P s i n 0. Consequently, the t o t a l cross section i s given by The maximum t o t a l cross section calculated using equation 6-4 and the d i f f e r e n t i a l cross section data of Stewart et a l (1964) and Berman et a l (1964) i s Eq 6-4 m a x <T (2-body) = 0 . 7 6 mb B E S T FIT CURVE OF <r=^rf~^ 3 V.dft\/9o\u00b0 PHOTON. ENERGY (MEV) FIGURE 2 0 Comparison of Total and Differential Cross Section Measurements -42-B \u00bb Theoretical Cross Section Calculations Berman et a l (1964) have obtained a good f i t to their 9 0 \u00b0 d i f f e r e n t i a l cross section data using an Irving wave function with size parameter 1\/^ M = 2o6 F as the ground state wave function for helium-3 (Chapter I I ) . They have considered only e l e c t r i c dipole absorption and consequently have under-estimated the t o t a l cross section by approximately 10% f o r photon energies greater than 20 mev. The Gaussian wave function f i r s t proposed by Yerde (1950) was rejected on the basis of th e i r data. I f the size parameter i n the Gaussian wave function i s chosen to f i t the maximum cross section, the p o s i t i o n of the peak i s too high i n energy; and i f the maximum i n the cross section i s f i t t e d to the oorrect energy, the corresponding cross section i s much too large to f i t the experimental data. From the work of Eichmann (1963), i t i s clear that the e l e c t r i c quadrupole contribution i s s i g n i f i c a n t and must be included i n transforming d i f f e r e n t i a l cross section data into t o t a l cross section values. Furthermore, f i n a l state i n t e r -actions would appear to Increase the maximum value of cross section by as much as 25% and cause the cross section to f a l l more r a p i d l y a t higher photon energies. As neither of these ef f e c t s have been considered by Beiman et a l , i t i s doubtful i f the theoretical f i t to th e i r data has much s i g n i f i c a n c e . Gorbunov and Varfolomeev (1964) attempt f i t s to t h e i r t o t a l cross section data using both Irving wave functions and the t h e o r e t i c a l estimations of Eichmann (1963). In neither case -43-i s there reasonable agreement between theory and experiment. In addition to e l e c t r i c quadrupole contributions and f i n a l state i n t e r a c t i o n s , Eichmann (1963) has included the mixed symmetry S' state with a 1% pr o b a b i l i t y i n the I n i t i a l state wave function for helium-3. Such an admixture i s expected to be present to account for the neutron capture by deuterium (Austern, 1952) and has the e f f e c t of decreasing the energy of the cross section maximum by 20% and increasing the maximum value of the cross section by 10%. The p o s s i b i l i t y of an admixture of D-state i n the ground state wave function of the 3-nucleon system has not been considered, although magnetic moment data c a l l f o r i t s i n c l u s i o n (Sachs, 1953). E l e c t r i c dipole absorption from the D-state to a continuum P-state would account fo r the iso t r o p i c component of the angular d i s t r i b u t i o n observed by Gorbunov and Yarfolomeev. To date, the deuteron wave function has been taken as a pure S-state although the measured quadru-pole moment of the deuteron indicates a 4% pr o b a b i l i t y f o r a D - 3 t a t e component. Furthermore, the f i n a l state \/interactions have Included only central forces; the influence of a tensor force on the f i n a l state wave functions has not been calculated. I t i s probable that a l l of these contributions to the cross section are s i g n i f i c a n t and must be Included i n further theoret-i c a l c a l c u l a t i o n s . C. Electron Scattering on Tritium and Helium-3. The electromagnetic structure of t r i t i u m and helium-3 -44-has been the subject of much recent experimental and th e o r e t i c a l i n v e s t i g a t i o n . Collard et a l (1963) have measured the charge density and magnetic moment form factors for both t r i t i u m and helium-3. The d i s t r i b u t i o n of magnetic moment f o r helium-3 i s more compact than that of charge, whereas the form factors f o r t r i t i u m appear to be approximately equal and furthermore equal to the magnetic moment fact o r f o r helium-3. The behavior of the form factors as a function of momentum transfer can be deduced from 3-nucleon wave functions. Several workers have attempted to f i t the data using various forms of wave functions f o r the ground state of the 3-nucleon system (Schiff et a l , 1963; Levinger, 1963; S c h i f f , 1964; Srivastava, 1964; Melster et a l , 1964; G r l f f y , 1964; Krueger and Goldberg, 1964). Several combinations of S 1 or D-state admixtures to the dominant S-state . with exponential, Gaussian and Irving wave functions y i e l d equally reasonable agreement with the experimental data. S c h i f f (1964) has proposed a 4% S'-state admixture to account for the difference i n oharge and moment form factors for helium-3. Krueger and Goldberg (1964) include a D-state admix-ture and G r i f f y (1964) indicates that a T = 3\/2 admixture to the dominant T = 1\/2 component i n the ground state wave function could also account f o r the difference i n form f a c t o r s . I t i s apparent that e x i s t i n g theoretical f i t s to the electron scattering data are too in s e n s i t i v e to determine 3-body wave functions. I t i s also evident that t h e o r e t i c a l calculations on the photodisintegration of t r i t i u m and helium-3 are f a r more -45-sensltive to the choice of ground state wave functions. D. Conclusions The experimental teohnique used in the present cross section measurements has the advantage of using monoenergetic photons. An extension of these measurements using the 17.6 mev 7 8 gamma ra d i a t i o n from the L i (p,fr)Be reaction would serve to d i f f e r e n t i a t e between the r e s u l t s of Gorbunov and Varfolomeev (1964) and the 90\u00b0 d i f f e r e n t i a l cross section data. The reaction could not be observed i n the i o n i z a t i o n chamber used i n the present work as the w a l l loss would be p r o h i b i t i v e . Prelim-inary calculations indicate that the experiment could be done using s o l i d state oounters. The 2-body photodisintegration cross sections at 8.06 and 9.17 mev agree very well with the cross section calculated from the inverse reaction D(p,tf\" )He 3 using the p r i n c i p l e of detailed Balance ( L a i , 1961; G. Bailey and G. M. G r i f f i t h s , private communication). The r e s u l t s also agree with the work of Bosch et a l (1964) on the photodisintegration of t r i t i u m and strengthen the hypothesis of charge independence of nuclear forces. The 3-body cross section for the photodisintegration of helium-3 at 9.17 mev i s found to be (0.25 \u00b1 0\u00ab13)mb, i n agreement with Gorbunov and Varfolomeev (1964). The 3-body energy spectrum did not show s i g n i f i c a n t deviation from the shape predicted by phase space calculations i n the region where -46-the sum of the proton energies i s greater than 1 mev. This would indicate that f i n a l state coulomb interactions f o r the 3-body breakup at a photon energy of 9.17 mev are not s i g n i f i -cant . - 4 7 -APPENDIX A Cross Section Calculation A. Chamber .Efficiency The number of photodisintegrations which occur i n the active volume of the i o n i z a t i o n chamber has been calculated by Robertson (1963). Consider a small element of volume dV i n the chamber, of area dA and thickness dx at a distance x from the gamma source. The areal density of helium atoms i n t h i s volume element is given by pHe^x where p^\u00a3 i s the atom density of helium i n the chamber. I f the attenuation i n passing through the gas between the source and volume element i s neglected, the number of gamma rays which pass through dV i s Ny. i s the t o t a l number of gamma rays emitted by the source with an angular d i s t r i b u t i o n 4-TT sWQoSons The number of photodisintegrations i n dV i s given.in terms of J i r . I ( c o s e ) = a Q + o ^ c o s e + a 2 c o s a e + . where -48-the cross section <T by tlx, K c o^eV^ ^ . \/ o .d* dA can be written as x2d5c where dSc i s the s o l i d angle subtended by dA at the source. The t o t a l y i e l d from the active volume i s Y i e l d = J \/ l f f ' ^ C 0 S Q y ) , < f ' PHV ^* * D ^ E Q A _ 1 Chamber Active Volume I f the source Is a perpendicular distance b 4- d from the chamber centre axis where b i s the radius of the chamber we define functions Hn(d) = || cosned5ld> C h a m b e r A c J i v e V o l u m e In terms of these functions, equation A - l becomes Yie l d = f \u2022 p H \u20ac ' ^  ' H ( d ) Eq A-2 where H(d) - a Q H 0(d) -f eL\u00b1 H-^d) 4- a 2 H 2(d)4 .... Robertson has evaluated H n(d) by numerical Integration for n = 0 , 2 , 4 - and BlacJtmore (private communication) has repeated the c a l c u l a t i o n with greater accuracy. The r e s u l t s f o r n = 0,2 are shown i n Figure 21.for the chamber at 90 to the d i r e c t i o n of the proton beam. I t should be noted that the graph given i n Robertson's thesis corresponding to Figure 21 i s Incorrect. B. Atom Density of Helium-3 In the course of the three years taken to investigate the cross section f o r the photodisintegration of helium-3, the gas mixture of argon, methane, and helium-3 was cycled i n and out of the chamber several times. During one period, the chamber developed a leak and part of the gas was l o s t . In a l l cases, when the gas was transferred, accurate pressure readings were taken using a March \"Master Test\", Model 210 pressure gauge so that the atom density of helium-3 was always known to within 1%, In c e r t a i n cases, the argon and methane were separated from the hellum-5 by freezing out these gases at a temperature of 65\u00b0K i n a trap cooled by s o l i d nitrogen. The vapour pressure of argon at 65\u00b0K i s 0.44 psia and t h i s r e s i d u a l pressure of argon was accounted for i n the pressure corrections. At the time of the 8.06 mev runs, the chamber contained 2,24 \u00b1 0.03 atmospheres of helium-3 at 20\u00b0C. This i s equivalent to an atom density of (6.02 \u00b1 0.08)(10) 1 9 atoms per cm 3. The pressure i n the chamber during the 9.17 mev 2-body di s i n t e g r a -t i o n runs was 1.515 \u00b1. 0.02 atmospheres and the atom density of helium-3 was (4.07 \u00b1 0 . 0 7 ) ( l O ) 1 9 atoms per cm3. Both of these figures were checked by repeating the work of Warren et a l \" T 0.1 0.2 0.3 0.4- 0.5 0.6 d\/v''3 FIGURE ?IQ CHAMBER AT 90 TO PROTON BEA.M DIRECTION FIGURE 21 b FIGURE 21 H Q(d) vs. d and H 2(d)\/H 0(d) vs. d for Chamber of Volume V and Diameter to Length Ratio 0.783 -50-(Appendix E) at 7.12 mev and using the known cross section at this energy to determine p H g . The agreement i s w e l l within the \u00b1 10% experimental error of the comparison measurement. During the 9.17 mev 3-body run the atom density of helium-3 at 20\u00b00 was (3.79 \u00b1 .04)(10) . G. Wall E f f e c t At a given gamma ray energy Ey. and f o r a fi x e d t o t a l density of gas i n the chamber, the photodisintegration products have a d e f i n i t e range, R. A f r a c t i o n of these produots w i l l c o l l i d e with the c y l i n d r i c a l wall or pass out of the active volume defined by the guard rings at the end of the chamber. The e f f e c t of th i s \"wall l o s s \" i s to remove counts from the f u l l energy peak at E Q = (E^ - Qj mev to a lower energy i n the spectrum. On the other hand, a f r a c t i o n of i o n i z a t i o n tracks which originate outside the sensitive volume w i l l extend into the active region. These events w i l l a l s o appear i n the low energy part of the spectrum and are termed \"end e f f e c t \" . The combination of the processes which add counts to the low energy section of the spectrum i s termed wall e f f e c t . 1. Wall Loss For an accurate measurement of the number of reactions occurring i n the active region, i t Is necessary to know the magnitude of the w a l l l o s s and i t s influence on the shape of the spectrum. Let the f r a c t i o n of tracks of length R cm o r i g i n a t i n g i n the a c t i v e volume which eith e r s t r i k e the wall or extend into the end region of the chamber be P(R). -51-For a cylinder of radius b cm and length L cm, Robertson (1963) has calculated P(R) to be He approximates the cylinder by a plane and shows thi s approximation to be v a l i d f o r R<b. He furthermore assumes an i s o t r o p i c d i s t r i b u t i o n of events and indicates that the value of P(R) i s not changed by a s i n O angular d i s t r i b u -tion (as i s expected for the photodisintegration products) providing P(R) < 0.5. The further assumption that the events are uniformly d i s t r i b u t e d throughout the chamber volume i s not as well j u s t i f i e d . The gamma f l u x through an element of volume dV i n the chamber a distance r from the source i s proportional to ' \/ r 2 \u2022 Hence the actual wall loss P 0(R) w i l l be greater than P(R) since the number of events taking place near the w a l l (close to the gamma source) w i l l be greater than f o r a uniform d i s t r i b u t i o n . Robertson has calculated the l i m i t s on P Q(R) for the geometry used i n the experiment. He finds 2, Spectrum Shape due to the Wall Loss A f r a c t i o n of the t o t a l number of counts i n the photo- ' dis i n t e g r a t i o n spectrum w i l l appear below the f u l l energy peak at energy E Q . Part of this low energy t a i l i s due to wall l o s s ; the f r a c t i o n P(R) of events i n the active volume Eq A-3 P ( R ) <-. P 0 ( R ) < (.12 P ( R ) -52-which c o l l i d e with the w a l l or extend into the end region of the chamber. The remainder of the t a i l i s due to end e f f e c t . In the 2-body breakup of helium-5, the proton and deuteron have energies 2E Q\/3 and E Q\/3 res p e c t i v e l y . I f the ranges are short compared to the wall curvature, only one of the reaction products can c o l l i d e with the w a l l . The maximum energy l o s t i n such a c o l l i s i o n i s 2E 0\/3. Alterna-t i v e l y , the end e f f e c t w i l l contribute counts from zero energy to a maximum energy of 2E Q\/3 i n the spectrum. Batchelor et a l (1955) discuss the shape of such a spectrum and these r e s u l t s are adapted by Robertson to the chamber used i n this experiment. Figure 22 shows the calculated wall loss spectrum shape for the 8.06 and 9.17 mev 2-body runs. The end eff e c t contribution i s not shown. The following assumptions were made i n the c a l c u l a t i o n . a. The curvature of the wall can be neglected. b. The track d i s t r i b u t i o n i s i s o t r o p i c . c. The reactions are uniformly d i s t r i b u t e d throughout the chamber. d. The stopping power dE\/dx i s constant. The f i r s t three approximations are as v a l i d for the spectrum shape c a l c u l a t i o n as they were f o r the wall loss c a l c u l a t i o n . The maximum w a l l loss correction was obtained f o r the 9.17 mev results and amounted to 29%. The error i n t h i s wall O a UJ (0 s: T O T A L W A L L L O S S P (R )= l5.9\u00b0\/\u00ab V of r . $ loo-i P A R T I A L W A L L L O S S P ( R ) - 6.5%, O.S56 \\.7\u00bb2 2.568 E N E R G Y ( M E V ) WALL L O S S S P E C T R U M F O R E ^ = 8 . 0 6 M E V i n \u00bb- ui Pi * \u00b05 ar ui CO o z ar H 5 or T O T A L W A L L L O S S P ( R ) = 2 9 % P A R T I A L W A L L L O S S P ' ( R ) \u2022 \\0.\u00b0) % 1654 1.226 2.4-52 3.677 E N E R G Y ( M E V ) W A L L LOSS S P E C T R U M F O R E Y e9- 1\" 7 M E V \/ FIGURE 22 Wall Loss Spectra for the Reaction He ( \u00a3 , p)D -53-loss correction i s (-22% - 10%) which would r e s u l t i n an error of (-6% \u00b1 3%) i n the t o t a l y i e l d . An energy dependent dE\/dx a l t e r s the shape of the spectrum within the energy i n t e r v a l s E 0\/3 to 2E Q\/3 and 2E 0\/3 to E 0 but does not appreciably change the number of counts i n each i n t e r v a l . To reduce the error i n the wall loss correction and to eliminate the effect of an energy dependent ^\/dx, the t o t a l y i e l d was calculated i n terms of a y i e l d f o r E > E 0\/3 and a p a r t i a l w a l l l o s s . This has the further advantage of removing the end e f f e c t from the c a l c u l a t i o n . \" 3. 2-body Photodisintegration Speotrum Analysis The method of spectrum analysis i s best explained with reference to the hypothetical spectrum shown i n Figure 23. K(E) i s the number of counts per u n i t energy so that the t o t a l number of counts N Q i s given by Due to the f i n i t e energy r e s o l u t i o n , the f u l l energy peak has a width 2 S E which buries a part of the w a l l loss spectrum i n the peak. We assume that the f i n i t e energy resolution does not a f f e c t the shape of the wall loss spee-trum to an appreciable degree. The number of counts i n the peak Kp, excluding the w a l l loss contribution, i s given by Eo+SE Eq A-4 E o \/ 3 -54-Eq A-5 where the wall loss removes N QP(R) counts from the peak. The actual number of counts i n the peak i s denoted by Np'. Np' i s the sum of Np and the wal l loss contribution to the peak. The wall l o s s contribution i s that f r a c t i o n of the t o t a l number of wal l loss counts f o r which the energy i s greater than E 0 - BE . This f r a c t i o n i s e s s e n t i a l l y the r a t i o of the area under the wal l loss spectrum f o r energy greater than E 0~ SE to the t o t a l area and i s given by 0 + \u00a3 0 \/ 3 Since the t o t a l number of wall l o s s events i s N QP(R), Np' i s given by Combining equations A-5 and A-6 and solving f o r N Q y i e l d s Equation A-7 gives the t o t a l y i e l d N Q i n terms of the measured number of counts i n the peak and the calculated -55-wall l o s s . In order to reduce the dependence of the t o t a l y i e l d on the calculated w a l l loss and spectrum shape, we calculate the t o t a l y i e l d i n terms of a y i e l d f o r E >2\"^'5\/3 and a p a r t i a l w a l l loss P*(R). P* (R) i s the f r a c t i o n of the t o t a l number of counts which appear i n the spectrum at an energy less than ^^\/^\u00bb P'(R) i s given by Hence the t o t a l y i e l d N 0 Is given by N 0 - - ^ N(E)^E + ( * \u00ae \u2022 N p Eq A-8 where Np i s given by equation A - 6 . The difference between the t o t a l y i e l d as calculated using equation A-7 and the t o t a l y i e l d calculated from equation A-8 was always l e s s than 2%. I t i s assumed that equation A-8 gives a more accurate value of the y i e l d . -56-APPENDIX B The Preparation of Carbon-15 Targets Commercially available C^3 targets are produced by separating the C-1-3 isotope i n a mass spectrometer and allowing 15 the C beam to h i t a target backing. This technique has certain inherent weaknesses. The C i s only loosely attached to the target backing and i s not able to withstand bombardment by proton beams greater than a few microamps. The targets so produced are non-uniform and consequently have a low y i e l d r e l a t i v e to the calculated y i e l d based on the measured target thickness. Further-more, the thickness of such targets i s l i m i t e d to a few kev f o r 'l mev protons. For these reasons i t was necessary to produce C 1 3 targets free of these shortcomings. P h i l l i p s and Richardson (1950) have reported a technique whereby benzene\"is thermally \"cracked\" on s i l v e r f o i l s using a high temperature oven. In an alternative procedure they used an induction heater to crack methyl iodide, CH 3I, on n i c k e l disks. Seagrave (1952) prepared carbon targets by passing current through a tantalum s t r i p i n a chamber containing CH^ or CHgl. Holmgren et a l (1954) and McCormick et a l (1961) report success with similar, techniques. The method used i n the present work i s simple, e f f i c i e n t , and reproducible. Methyl iodide, enriched to 59.5% 13 C was obtained from Merck, Sharp and Dohme of Canada Limited. The CHgl was purchased i n a sealed glass container (11) which was -57-f i t t e d with a flanged pyrex top and attached to the apparatus shown i n Figure 24. The apparatus consisted of a valve assembly (8); (9), (10) and a pyrex tube (7) i n which a 0.002 i n thick platinum s t r i p was suspended (6). The platinum s t r i p was heated by ac current from a 5 v o l t i s o l a t i n g transformer fed by a 110 volt v a r i a c . The output of the transformer was connected to the Kovar seals (1) and the brass plate (15). The apparatus was made vacuum tight by means of a neoprene 0-ring(2) and a flange assembly (5),(4). The procedure used for making targets i s outlined below. 1. A clean platinum s t r i p 1.4 cm wide x 7.5 cm long was spot welded to 0.040 i n . n i c k e l wire (5) and to a n i c k e l plate (12) and suspended i n the pyrex tube. 2. The tube assembly was evacuated to a pressure of 2(10) mm, of Hg. through a pumping port (13) and the platinum was outgassed at 800\u00b0C (red heat) by passing 40 amperes ac current through i t . 3. The tube was closed to the pump and the valve to the CHgl was also closed. For the f i r s t target, the f r a g i l e glass seal on the v i a l containing the CHgl was broken using an i r o n rod held within the tube with a permanent magnet. This allowed the volume of tube up to the Viton A valve diaphragm to become saturated with CH I vapour at a pressure of 30 cm of Hg. FIGURE 24 Target Preparation Apparatus. Scale - Full Size -58-4. With the platinum heated to 600\u00b0C ( d u l l red heat), the valve to the CH 3I was opened and the vapour diffused into the craoking chamber. Thermal decomposition of the CHgl proceeded s a t i s f a c t o r i l y and the carbon deposited on the platinum. The copious quantities of gaseous iodine released i n the process did not condense on the hot platinum but deposited on the sides of'the pyrex tube which was cooled with an a i r blower. Aft e r 5 minutes of cracking, the valve to the CHgl was closed and the iodine was pumped o f f . This procedure could be repeated many times, depending upon the thickness of target desired. Each f i v e minute run deposited about 100 micrograms\/cm 2 of carbon on each side of the platinum i n the form of an extremely tough layer. I f the platinum was cooled quickly, the carbon layer b l i s t e r e d and could be removed from the platinum i n t a c t . I f the platinum was cooled slowly, the carbon adhered to the platinum which then served as a target backing. Approximately 45% of the carbon i n the CHgl was deposited on the platinum. The \"one run\" targets were 10 to 15 kev thick to 1.8 mev protons and withstood beam currents of 35 micro amps f o r hundreds of hours when suitably cooled. The exc i t a t i o n function f o r such a target i s shown i n Figure B5. The maximum y i e l d i s 7.4 gemma rays of energy 9,17 mev per \/ * 9 (10) protons* This compares favourably with the t h e o r e t i c a l 1.740 1.750 1.7(60 1.770 P R O T O N E N E R G Y ( M E V ) FIGURE 25 Yield of 9.17 mev Gamma Rays as a Function of Proton Energy -59-g y i e l d of 7.5 gamma rays per (10) protons as calculated using the measured cross section and resonance width (Appendix C). A C 1 5 target 600 kev thick to 1 mev protons was prepared by peeling the carbon o f f the platinum and placing several layers i n a gold target holder. This target produced a maximum y i e l d of 5.8 photons of energy 8,06 mev per (10) 9 protons of energy 730 kev. The y i e l d calculated from the measured cross section and resonance width i s 6.0 photons per 9 (10) protons. -60-APPENDIX C The. Reaction C 1 3 ( p , ) N 1 4 and the  Measurement of the Gamma Flux A. Gamma Ray Counter E f f i c i e n c y The measurement of the e f f i c i e n c y of the 2-3\/4 i n . diameter by 4-| i n . long Nal(Tl) s c i n t i l l a t i o n counter i s discussed by Singh (1959), G r i f f i t h s et a l (1962), Larson (1957) and Robertson (1963). The gamma counter e f f i c i e n c y f o r gamma rays of energy Ey> i s given i n terms of the number of counts i n the gamma spectrum above an energy bias E^\/2 r e l a t i v e to the t o t a l number of gamma rays impinging on the counter. The \u2022effic i e n c y i s w r i t t e n \u00a3(E Y ; E^ > \/2) and i s shown i n Figure 26 as a function of Ey \u2022 Robertson (1963) derives expressions for the e f f i c i e n c y i n terms of an energy bias other than Ey. \/2, and th i s straightforward c a l c u l a t i o n w i l l not be repeated here. There i s one ess e n t i a l difference between the work of Robertson (1963) and the present work. The absolute e f f i c i e n c y of the s c i n t i l l a t i o n counter had been measured at a photon energy of 6.14 mev and could be extrapolated to 6.92 and 7.12 mev with l i t t l e e r r o r . Such extrapolation i s not s u f f i c i e n t l y r e l i a b l e for the 8.06 and 9.17 mev gamma rays used i n the present experiment, and the factor which l i m i t s the accuracy of the photodisintegration cross sections at these energies i s knowledge of the gamma counter e f f i c i e n c y . I t would be worth-while therefore, to measure the e f f i c i e n c y of the gamma counter FIGURE 26 Gamma Counter Efficiency for Half Energy Bias - 2 3\/4 in diam. by 4 1\/2 i n Long Nal(Tl) Crystal -61-at an energy greater than 6.14 mev. This could be done in the following way. Two steps are required. F i r s t l y , the absolute efficiency of the counter could be measured at 4.433 mev by counting the gamma rays to the ground state of C 1 2 from the f i r s t excited state at 4,433 1 5 1 2 * mev. This level can be populated by the reaction N (p,\u00b0<)C \u2022 The gamma yield from the consequent de-excitation can be determined exactly by counting the associated alpha particles with a sol i d state counter, providing the alpha and gamma angular distributions and the alpha-gamma angular-correlation are taken into account, l ? Secondly, one could populate the 16.11 mev level in C by the proton bombardment of at the well-known 160 kev resonance. This level decays 90% hrough the 4.433 mev level mentioned above, and gamma rays of energy 11.7 and 4.43 mev can be observed in coincidence. Hence the determined efficiency at 4,43 mev would lead directly to an experimental measurement of the efficiency at 11,7 mev. B, The Reaction C 1 5(p, T )H 1 4 as a Source of Gamma Rays 1\u00ab Introduction In order to obtain an accurate measurement of the cross section for the photodisintegration of helium-3 at gamma ray energies of 8.06 and 9,17 mev, we must know the angular distributions and relative intensities of the gamma rays produced by the proton bombardment of C ^ 5 at the 0,554 -62-and 1,75 mev resonances. As i s shown i n Appendix A, the angular d i s t r i b u t i o n has a large e f f e c t on the fact o r H n(d) which enters d i r e c t l y i n t o the cross section c a l c u l a -t i o n . The r e l a t i v e i n t e n s i t i e s of cascade gamma rays must be known In order to calculate the 8,06 or 9,17 mev gamma flux from the recorded gamma spectra. 2, 0,554 mev Resonance The reaction C^Cp,^ )N\"*\"4 was f i r s t studied, by Curran et a l (1939), They observed a resonance i n the gamma y i e l d at a proton energy of 0,57 mev and determined the maximum energy of gamma ray to be 8.5 mev. Subsequent work by Lauritzen and Fowler (1940), Fowler et a l (1948), and Seagrave (1952) fixed the energy of the resonance at 0,554 mev and the energy of the gamma ray to the ground state of at 8.06 mev, Seagrave also measured the resonance width PR and obtained a value of 32,5 kev. Devons and Hine (1949) measured the angular d i s t r i b u t i o n of the 8.06 mev gamma rays from the 8,06 (.554)- mev l e v e l and found i t to be i s o t r o p i c . This i s consistent with the l e v e l being formed by S-wave protons as expected. Subse-quent workers have Investigated the de-excitation of the 8,06 (.554)- mev l e v e l i n d e t a i l (Woodbury et a l , 1953; Hird et a l , 1954; Lehman et al,1956; Wilkinson and Bloom, 1957; Broude et a l , 1957). The accumulated data has been compended by Ajzenberg-Selove and Lauritzen (1959) and i s -63-shown i n Figure 27. 3. 1,75 mev Resonance Day and Perry (1951) found a sharp resonance i n the reaction C 1 3(p,}f ) N 1 4 at a proton energy of 1.75 mev, y i e l d -ing 9.17 mev gamma rays. Several workers (Table XII) have since measured the angular d i s t r i b u t i o n s or the anisotropy A f o r the 9.17 mev to ground state t r a n s i t i o n . The r e s u l t s of Rose et a l (1960) are used i n t h i s present work. TABLE XII Measured Angular D i s t r i b u t i o n of the 9.17 mev Radiation at the 1.75 mev resonance Angular D i s t r i b u t i o n Anisotropy = Yield(0\u00b0) - i Yield(90\u00b0) Day and Perry (1951) Woodbury et a l (1953^ Rose et a l (1960) Segal et a l (1961) 1 - (0.55\u00b1 0.02)cos 2 e \\Q+\\ <0.02 1 - (0.59 \u00b10.03)oosf 6 + (0,03 \u00b1 0.03)cos*G - 0.399\u00b1 0.013 - 0.48 \u00b10.03 - 0.55+0.02* - 0.56\u00b1 0.04* ^Calculated from the. measured angular d i s t r i b u t i o n . Several people have measured the r e l a t i v e i n t e n s i t i e s of the cascade gamma rays produced In the de-excitation of the 8.06-5.69-4-.9I -3.95-2.31-CM 00 t \u2014 r in m vO X 8.0k M E V L E V E L D E C A Y (O) ! + 9 . 1 7 -4-7.03-6.44-5.Q3. 5.69-5.10-3.95-231 SQI CM VI +\u00bb ort CM +\u2022 0D m o m N 1 * 9.17 M E V L E V E L D E C A Y 3 FIGURE 27 Decay Schemes f o r the 8.06 and 9.17 mev Levels of N x . Only those le v e l s involved i n the decay of the 8.06 and 9.17 mev states are shown. Broken arrows denote uncertain t r a n s i t i o n s and parentheses denote uncertain assignments. -64-9,17(1*75)-mev resonanoe l e v e l i n N 1 4 (Seagrave, 1952; Wood-bury et a l , 1953; Rose et a l , 1959; Rose, 1960), The re s u l t s of Rose (I960) are reproduced i n Figure 27 and are used i n the ca l c u l a t i o n of the gamma flux i n the present work, 4. Doppler S h i f t When a nucleus i n an excited state of energy E Q , moving with v e l o c i t y v, decays by emission of a gamma ray to the ground state, the energy of the gamma ray i s given by Eq C I where 14 i s the mass of the nucleus and 0 i s the angle between v and the dir e o t i o n of emission of the gamma ray. The f i r s t term i n equation C - l i s the Doppler s h i f t , the second term i s the r e c o i l s h i f t , For the decay of the 9,17 14 mev excited state i n N , the r e c o i l s h i f t i s 3,2 kev. Since the i o n i z a t i o n chamber was placed at 90\u00b0 to the proton beam and hence to ^ , the Doppler s h i f t i n the present case i s zero. The maximum Doppler s h i f t occurs at 8 = 0 \u00b0 or 180\u00b0 and when v has the maximum value allowed by the kinematics of the reaction; that i s , when decay takes place before the -65-nueleus slows down i n the target. The magnitude of t h i s maximum s h i f t for the decay of the 9.17 mev state i s \u00a3 40 kev. A knowledge of the stopping time X and the stopping oross section \u00a3 f o r the nucleus leads to a direct measure-ment of the l i f e t i m e of the excited state. Such a s h i f t i n gamma ray energy would r e s u l t i n a corresponding s h i f t i n the 2-body photodisintegration peak i n the i o n i z a t i o n chamber. However, the expected s h i f t f o r the 9.17 mev gamma rays i s too small to be observed and an estimate of the l i f e t i m e of the state i s not possible by this technique. C. Analysis of the Gamma Spectra  0*554 mev Resonanoe The gamma spectrum obtained by bombarding the thick target described i n Appendix B with 0.730 mev protons i s shown i n Figure 28. The de-excitation of the 8.06(.554)-mev 14 l e v e l i n N y i e l d s 8.06, 5.7 and 4.11 mev gamma rays i n the r a t i o 82:11:4. The 5.7 mev ra d i a t i o n i s due to the sum of the 5.69 -*-0 and 8.06->-2.31 tran s i t i o n s which cannot be separated i n the s c i n t i l l a t i o n counter spectra. Any aniso-tropy i n the 5.7 mev component can be neglected at the angle of observation used i n the present work. The t o t a l number of counts above 4.03 mev In the spectrum shown i n Figure 28 i s given by M * [o.82\u00a3(8.O6;4:0B) + 0.O4r\u00a3(5j;4-.03)-\u00bb-OJl\u00a3(4.l\\;4:O5)]N' NUMBER OF COUNTS -66-where ^ ( E ^ ; E b ) i s the s c i n t i l l a t i o n counter e f f i c i e n c y f o r gamma rays of energy E ^ at an energy bias E ^ and N ' i s the t o t a l number of 8.06, 5.7 and 4.11 mev gamma rays impinging on the counter. \u00a3(5.7;4.03) was determined using the e f f i c i e n c y to a ha l f energy bias, \u00a3(5.7; 2.85) 3and an assumed spectrum shape. The gamma ray spectrum from the 340 kev resonance of the reaction F 1 9(p , \u00a9 0 n o 1 6 which y i e l d s 98% 6.14 mev radi a t i o n (Dosso, 1957) was assumed to give the shape of the spectrum f o r the 5.7 mev rad i a t i o n and i s shown i n Figure 29. The r a t i o of the number of counts above 4.03 mev to the number above 2.85 mev was 0.82 \u00b1 0.01. Hence \u00a3(5.7; 4.03) i s given i n terms of the e f f i c i e n c y to a half energy bias of 2.85 mev by E(5.7;4-.03)= 0.82 \u00a3(5.7; 2.85) = 0.6OB \u00b1 0.008 where \u00a3,(5.7; 2.85) i s given by Figure 26. The uncertainty i n \u00a3(5.7; 4.03) does not include the systematic error i n \u00a3 (5.7; 2.85). As seen In Figure 28, the 4.11 mev rad i a t i o n i s e a s i l y accounted f o r by extrapolation of the 8.06 and 5.7 mev t a i l , again using an assumed spectrum shape. The r a t i o of the number of counts above 4.03 mev contributed by the 4.11 mev ra d i a t i o n to the t o t a l number above 4.03 mev was found to be 0.023 \u00b1 0.003. Hence the r a t i o of the number of counts above 4.03 mev due to the 8.06 mev ra d i a t i o n to the t o t a l I IOO -, E N E R G Y ( M E V ) FIGURE 29 6.14 mev Gamma Spectrum from the Reaction F 1 9 ( p,=*Y)016 at the 340 kev Resonance -67-number above 4.03 mev i s 1 - 0.04 \u00a3(5.7}4.03) - 0.023 - 0,953 \u00b1 0,011 The number of 8,06 mev gamma rays incident on the counter i s given i n terms of the number of counts N above 4,03 mev in the spectrum by ^ c o u ^ T e r _ 0 . 9 5 3 N 8 - 0 G E(8.06;*h03) = \\.2B Kl 2, 1.75 mev Resonance 13 The gamma spectrum from the proton bombardment of C at 1.75 mev i s shown i n Figure 30. As well as the primary component at 9,17 mev, the speotrum contains contributions from 7,03, 6,44, 5,7 and 5,1 mev gamma rays. In order to determine the number of 9,17 mev gamma rays from the spec-trum the contribution from the other gamma rays must be subtracted. Two methods of subtraction were used. In the f i r s t case, the 9,17 mev contribution was assumed to have the same shape as the pure 8.06 mev spectrum obtained previously. Using this shape and the known efficiency \u00a3,(9.17; 4,585), the number of 9,17 mev gamma rays incident on the counter is given in terms of the number of counts N above 4,585 mev by Sooo 4ooo Y-z 3ooo-o (J 2ooo I ooo B I A S I 1 1 1 1 1 1 1 1 1 90 l O O U O I20 <3o 14-0 150 1 6 0 170 \\QO KlCKSORTER C H A N N E U i 1 1 1 1 1 1 1 1 1 1 1 5 6 7 8 9 10 E N E R G Y ( M E V ) FIGURE 30 Gamma Spectrum from the Reaction C 1 3 ( p , Y ) N 1 4 at the 1.75 mev Resonance -68-counter N = 1.156N 9.17 In the second method, the e f f i c i e n c i e s \u00a3(E\u00a3;4\u00ab585) f o r each gamma ray were calculated using the known e f f i c i e n c i e s EfE^E^y^) as given i n Figure 26 and assuming the spectrum shape to be as given i n Figure 29. In terms of the r e l a t i v e i n t e n s i t i e s R^O) of the gamma rays a t an angle \u00a9 to the proton beam, the number of 9.17 mev gammas incident on the counter i s given by 2 R t(e) \u00a3 ( E i ; 4-.SS5) R 9. l 7(e) \u00a3(ai7;+.505) Table XIII shows the values of E^tG) and (E i;4.585) as calculated. Using these values one obtains, counter N - 1.162N 9.17 The two methods are i n good agreement and a value counter N = 1.16N was used i n c a l c u l a t i n g the 9.17 mev 9.17 gamma f l u x . N counter 9.17 TABLE XIII Angular Distributions, Relative Intensities and Scintillation Counter Efficiencies for the Gamma Rays from the 9.17(1.75)-mev Resonance Level in N-Gamma Ray Energy, Ej. Angular Distribution Relative Intensity integrated over 4 TT steradians R i ( G ) 9=152.3\u00b0 \u00a3(Ei ; f ) \u00a3(E i ; 4.585) 9.17 1 - 0.55cos28 100 70 0.782 0.782 7.03 isotropic 3 3 0.767 0.662 6.44 1 + 1.6cos 2\u00a9 - l.lcos^\u00a9 7 8.5 0.76 0.606 5.7 1 - 0.55cos2\u00a9 3 2.1 0.744 0.518 5.1 1 - 0.32cos 2e 3 2.5 0.728 0.223 -69-APPENDIX D Neutron Induced Background and Neutron Shielding One of the main experimental d i f f i c u l t i e s associated with the measurement of the cross section f o r the photodisin-tegration of helium-3 was the problem of neutron-Induced back-ground. The reaction He (n,p)T has a po s i t i v e Q-value of 0.765 mev. The cross section as a function of neutron energy i s shown i n Figure 31. Because of the high cross section and beoause of the unique energy release f o r t h i s reaction, several workers have used helium-3 f i l l e d Ionization chambers and proportional counters as neutron spectrometers (Batchelor et a l , 1955; M i l l s et a l , 1962; Freeman and West, 1962; Brown, 1964; Sayres and Coppola, 1964; Friedas and Chrien, 1964). As discussed i n Chapter IV, the thermal neutron capture by helium-3 served as an energy c a l i b r a t i o n f o r the io n i z a t i o n chamber. The neutron disintegrations were dis t r i b u t e d through-out the chamber and produced counting conditions s i m i l a r to those met i n the photodisintegration measurement. In a l l other respects, the advantages of the chamber as a neutron detector became disadvantages f o r the photodisintegration work. For the 2-body photodisintegration at 8.06 and 9.17 mev, the thermal neutron capture peak at 0,765 mev d i d not i n t e r -fere with the photodisintegration spectrum. Hence f a s t neutron d i s i n t e g r a t i o n r e s u l t i n g i n an energy release i n the chamber of greater than 1.5 mev was the only source of neutron Induced FIGURE 31 Cross Section for the Reaction He ( n, p)T. From Hughes and Schwartz (1958) -70-background whioh proved troublesome. Elaborate p a r a f f i n and cadmium shielding eliminated t h i s background. The neutrons were moderated by the p a r a f f i n and absorbed by the cadmium which has a high capture cross section f o r thermal and epithermal neutrons. For the 3-body photodisintegration at 9.17 mev, the thermal neutron peak f e l l i n the middle of the 3-body spectrum (Figure 1, Chapter I I ) , and a l l neutrons, thermal or f a s t , i n t e r f e r e d with the measurement. The main source of neutrons, and that most e a s i l y eliminated, was i n the e x i t seotion of the Yan de Graaff column and i n the 90\u00b0 analyzing magnet vacuum box where the neutrons were produced by the deutron bombardment of deuterium and carbon. The deuterons a r i s e from the 0.0156% natural deuterium contamina-tion of the hydrogen used i n the Yan de Graaff ion source whioh res u l t s i n deuterium ions being accelerated along with the proton beam. The 90\u00b0 analyzing magnet selects the mass one proton beam; the mass two and mass three beams (Hg, D and HD ) s t r i k e a tantalum s t r i p i n the magnet box (Figure 32). The number of neutrons produced i n the column and magnet box was kept to a minimim by p e r i o d i c a l l y cleaning the tantalum collimator i n the accelerating column and the tantalum beam catcher i n the magnet box. The neutrons which were produced were prevented from entering the chamber by wax shielding walls and a wax and cadmium castle around the chamber and target. For the 8.06 mev runs at a proton energy of 0,730 mev, the proton beam i t s e l f produced no neutrons and the precautions MASS 2 BEAt-1 J IONIZATION CHAMBER V A N O E . G R A A F F C O L U M N T A N T A L U M . C O L L I M A T O R 90 A N A L Y Z I N G M A & M E T | T A N T A L U M C O L L I M A T O R S ' W A X A N D C A D M I U M C A S T L . E WAX AMD CAOMIUM WALL 5 r PLATlWut TUBE LlNf E L & C T R O S T A T I F O C U S S I N G P R O T O N B E A M T A N T A L U M B E A M C A T C H E R PYRE.H. T U B E \" C O L D T R A P C A R B O N - 13 ON PLATINUM T A R G E T R A C K I N G FIGURE 32 Beam Collimators and Neutron Shielding -71-outlined above were adequate. However, f o r the 9.17 mev runs, the proton beam energy was 1.75 mev, we l l above the (p,n) threshold f o r most materials, as shown i n Table XIV. By introduc-ing collimators i n the ho r i z o n t a l pyrex beam tube, the proton beam was prevented from s t r i k i n g the glass, a major source of neutrons from (p,n) reactions. In a s i m i l a r manner, the proton beam scattered o f f the platinum target backing was shielded from the beam tube w a l l by a 0.001 inch thick tantalum l i n e r . Such extra precautions e f f e c t i v e l y eliminated a l l neutrons which resulted i n an energy release i n the chamber greater than 1.5 mev and thus were adequate f o r the S-body photodisintegration at a photon energy of 9.17 mev. Such was not the case f o r the 3-body runs at 9.17 mev. A l l attempts to completely eliminate the thermal neutron peak f a i l e d . Table XIV shows that there are very few materials suitable f o r use as a target backing, as beam collimators, or as a beam tube l i n e r f o r which the (p,n) threshold i s less than -1.75 mev. Carbon and n i c k e l are obvious choices. However, impurities i n both materials produced a neutron f l u x which resulted i n 20 thermal neutrons counted by the chamber per 15 (6)(10) protons incident on the material. The concentration of impurities need not be greater than one part i n (10) to account for t h i s neutron count r a t e . The i o n i z a t i o n chamber i s \"black\" to thermal neutrons and the observed neutron count rate represents a thermal neutron f l u x of only 0.1 neutrons per cm per minute through the chamber for the proton beam currents used. TABLE XIV (p,n) Q-values. Calculated from the Mass Values of Everling et al (i960) Isotope % Natural Abundance (p,n) Q-value Isotope % Natural Abundance (p,n) Q-value Isotope X Natural Abundance (p,n) Q-value L i 7 92.48 -1.646 Mg 2 6 11.3 -4.808 C a 4 2 0.64 -6.660 Be9 100 -1.854 Al 2 ? 100 -5.607 C a 4 4 2.13 -4.432 B10 18.83 -4.56 S i 2 8 92.28 -14.545 Sc45 100 -2.827 BH 81.17 -2.764 Si 2? 4.67 -5.745 1^ 46 7.95 -8.082 C12 98.89 -18.453 p31 100 -6.219 T i 47 7.75 -3.695 C13 1.11 -3.003 S32 95.06 -13.812 T i 4 8 73.45 -4.805 N i 4 99.6 -5.934 S33 0.74 -6.231 Ti49 5.51 -1.383 016 99.8 -16.360 S34 4.18 -5.774 T i 50 5.34 -2.991 F19 100 -4.038 C I 3 5 75.4 -6.039 V51 99.75 -1.534 Ne 2 0 90.5 -16.121 C I 3 7 24.6 -1.598 C r 5 0 4.41 -8.433 N e22 9.2 -3.622 A 4 0 99.6 -2.274 C r 5 2 83.46 -5.485 Na 2 3 100 -4.875 K39 93.1 -7.638 C r 5 3 9.54 -1.370 Mg 2 4 78.6 -14.80 K41 6.9 -1.220 Cr5 4 2.61 -2.15 Mg 2 5 10.1 -5.074 C a 4 0 96.92 -14.768 Mn 5 5 100 -1.014 TABLE XIV (continued) Isotope % Natural Abundance (p,n) Q-value Isotope % Natural Abundance (p,n) Q-value Isotope % Natural Abundance (p,n) Q-value F e 5 4 5.90 -9.622 Ga 6 9 60.0 -3.02 Z r 9 6 2.8 -0.500 F e56 91.52 -5.383 Ga 7 1 40.0 -1.015 Nb 9 3 100 -1.265 F e 5 7 2.245 -1.649 Ge 7 0 20.45 -7.32 Mo 9 2 15.05 -7.200 Cc59 100 -1.857 Ge 7 2 27.41 -5.143 Mo 9 4 9.35 -5.102 N i 5 8 67.8 -9.317 Ge?3 7.77 -1.155 Mo 9 5 15.78 -2.439 N i 6 0 26.2 -6.912 Ge?4 \u2022 36.58 -3.347 Mo96 16.56 -3.760 N i 6 1 1.2 -3.076 Ge 7 6 7.79 -1.760 Mo9? 9.60 N.C. N i 6 2 3.7 -4.62 A s 7 5 100 -1.648 Mo 9 8 24.60 -2.500 N i 6 4 1.1 -2.46 B r 7 9 50.57 -2.404 M o 1 0 0 9.68 N.G. C u 6 3 69.1 -4.149 B r 8 1 49.43 -1.030 R h 1 0 3 100 -1.342 C u 6 5 30.9 -2.131 Rb85 72.15 -1.890 Pd102 0.8 N.C. Z n 6 4 48.87 -7.84 Rb8? 27.85 -0.510 p d104 9.3 -5.062 Z n 6 6 27.62 -5.96 Z r90 51.46 -6.900 p d105 22.6 -2.800 Z n 6 7 4.12 -1.781 Z r 9 l 11.23 -2.380 P d106 27.1 -3.753 Z n 6 8 18.71 -3.70 Z r 9 2 17.11 -2.860 P d108 26.7 -2.619 Zn70 0.69 -1.435 Z r 9 4 17.40 ^1.550 P d110 13.5 -2.230 TABLE XIV (continued) Isotope % Natural Abundance (p,n) Q-value Isotope % Natural Abundance (p,n) Q-value Isotope % Natural Abundance (p,n) Q-value Agl07 51.35 -2.223 SnU? 7.67 -2.602 W184 30.64 N.C. A g 1 0 9 48.65 -0.940 S n 1 1 8 23.84 N.C. W186 28.64 -3.300 Gdl\u00b0 6 1.22 N.C. S n 1 1 9 8.68 -1.361 Pt-192 0.78 -4.020 C d 1 0 8 0.89 -5.880 S n 1 2 0 32.75 -3.505 P t 1 9 4 32.8 -3.348 C d 1 * 0 12.43 -4.742 S n 1 2 2 4.74 -2.37 P t 1 9 5 33.7 -1.053 CdUl 12.86 -2.020 S n 1 2 4 6.01 -1.380 P t 1 9 6 25.4 -2.570 C d 1 1 2 23.79 -3.398 Sb*2* 57.25 -0.399 P t 1 9 8 7.23 -1.440 CdH3 12.34 -0.473 S b 1 2 3 42.75 -0.820 A u 1 9 7 100 N.C. CdH4 28.81 -2.203 jl27 100 -1.480 P b204 1.37 -5.068 G d 1 1 6 7.66 -1.370 C s l 3 3 100 -1.273 p b206 26.26 -4.383 I n 1 1 3 4.16 -1.466 C e 1 4 0 88.45 -4.042 P b207 20.82 -3.183 I n 1 1 5 95.84 -0.282 C e 1 4 2 11.1 -1.480 p b208 51.55 -3.659 Sn l l 2 1.01 N.C. P r 1 4 1 100 -2.582 B i 2 0 9 100 -2.68 S n 1 1 4 0.68 N.C. T a 1 8 1 100 -0.982 y238 99.28 -0.633 S n 1 1 5 0.35 N.C. W182 26.31 N.C. S n 1 1 6 14.28 -5.48 W183 14.28 N.C. -72-Of a l l the materials used as collimators and target backings, gold, platinum and reactor grade graphite produced the lowest neutron count rate i n the chamber (20 thermal neutrons per milliooulomb of proton beam on target) . Stopping the proton beam outside the castle reduced the count rate to less than 100 neutrons per coulomb of stopped beam. The number of neutrons produced by (\u00a3 ,n) reactions i n the material surrounding the target and chamber was at least an order of magnitude lower than those produced by (p,n) reactions. That i s , the presence of a 9.17 mev gamma f l u x did not increase the neutron f l u x to a measurable extent over the neutron f l u x observed with no gamma rays. The 3-body spectrum shown i n Chapter V was obtained using a platinum target backing and a platinum beam tube l i n e r . A self-supporting carbon-13 target would allow the proton beam to pass through the target and be stopped outside the c a s t l e . Preliminary runs with no target but with the beam passing through the castle indicate that neutron count rates of less than 200 neutrons per coulomb of proton beam can be attained. APPENDIX E Reprinted from T H E P H Y S I C A L REVIEW, Vol. 132, No. 4, 1691-1692, 15 November 1963 Printed in U. S. A. Photod i s in teg ra t ion of H e 3 nea r the T h r e s h o l d * J . B . W A R R E N , K . L . E R D M A N , L . P . R O B E R T S O N , ! D . A . A X E N . J AND J . R . M A C D O N A L D J Physics Department, University of British Columbia, Vancouver, British Columbia, Canada (Received 1 July 1963) The total cross section for the reaction He3 (y,p)T> has been measured at gamma-ray energies of 6.14, 6.97, and 7.08 MeV. The cross section was found to be 0.102, 0.298, and 0.307 mb at the three energies. The experimental cross-section values are compared with those of the inverse reaction D(p,y)Hc?, as an accurate check on the principle of detailed balance. TH E photodisintegration of He 3 has been observed by Cranberg1 and Berman et al? This letter describes the measurement of the total cross section of the reaction He3(Y,\/>)D (Q=\u2014 5.493 MeV) at gamma-ray energies of 6.14, 6.97, and 7.08 MeV. The experi-mental cross-section values are compared with those of the inverse reaction as an accurate check on the principle of detailed balance. The reaction was observed in a cylindrical, gridded ionization chamber of active volume 1.485 liters. The chamber contained 1.05 atm of He 3 , 0.0187 atm of methane, and 1.36 atm of argon. The methane was added to reduce the resolving time of the chamber to less than 2 usee, whereas the argon served as a stopping gas for the photodisintegration products. It was necessary to reduce the tritium contamination in the He 3 to eliminate the electron background due to the \/3 decay of tritium. The tritium contamination was reduced from one part tritium per 106 parts He 3 to five parts tritium per 1010 parts He 3 by freezing the tritium at 4 .2\u00b0K. The charac-teristics of the ionization chamber and the purifica-tion technique will be published in a separate communication.3 Two identical chambers were used in the experiment and were placed symmetrically on either side of the gamma-ray source. One chamber contained He 3 , methane, and argon, the other contained He 4 , methane, and argon. The outputs of the two chambers were fed through separate amplifying systems into separate halves of the memory of a model N D 103 Nuclear Data pulse-height analyzer. In this way, all effects not specific to the He 3 could be monitored. Elaborate wax and cadmium shielding was required to attenuate the thermal neutron background and thus reduce the cap-ture of thermal neutrons by the He 3. The gamma rays were produced by bombarding CaFs targets with protons accelerated by a 3 MeV Van de Graaff generator. Table I shows the relative yields and F I G . 1. Photodisinte-gration spectra. 1 3 0 1 120 IIO IOO 9 0 SO-TO 60 80 40 SO 20 IO-I 0.5 6 7 3 . 5 KEV RESONANCE 995 KEV RESONANCE He3+ Y '7.12 M \u00ab V I 1.0 I 1.5 '\u2022>.\u00ab\u2022'\u20ac N ERG Y IN M E V * Research supported by a grant from Atomic Energy ,of panada, Ltd. t Holder of a National Research Council Studentship 1960-:<>2f.Present'address: Rutherford High,Energy Laboratory, Oxford, England. ' \u2022''\u2022*'\u00a3\u2022'\u2022;'. \u2022 \u2022 ' \"\"; \" '\u2022' J's'iSi?.\/ i Holder of a National Research Council Studentship 1961-63. 1 L. Cranberg, Bull. Am. Phys. Soc. 3, 173 (1938).\" \u00abi. \u2022-.\u2022..->:,\u2022>-- ...... 8 B. L. Berman, L. J. Koester, Jr., and J. H. Smith, Phys. Rev. Letters 10, 527 (1963). ' K. L. Erdman, L. P. Robertson, D. A. Axen, and J. R. MacDonald, Can. J. Phys. (to be published). 1691 1692 W A R R E N , E R D M A N , R O B E R T S O N , A X E N , A N D M A C D O N A L D 0.5 l.o I.S ^ R E A C T I O N * [ E Y \" 5 . 4 9 3 ] M E V F I G . 2. Comparison of cross sections for the inverse reactions Ke?(y,p)T) and D(p,y)Ke'. angular distributions of the gamma rays from the reac-tion F 1 9 ( ^ , a 7 ) 0 1 6 at the two proton bombarding energies used i n the exper iment . 4 - 6 T A B L E I. Relative yields and angular distribution of gamma rays. - ^ p r o t o n (keV) Relative gamma-ray yields 6.14 6.92 7.12 MeV MeV MeV p\u2014y angular distribution 873.5 73% 20% 7% 6.14 MeV 1-0.1 cos^fl 6.92 MeV 1+0.51 cos=0-O.22 cos'0 7.12 MeV 1+0.622 cosV 935 75% 3% 22% Isotropic at all energies \u00abJ. M. Freeman, Phil. Mag. 41, 1225 (1950). 6 H. J. Martin, \\V. A. Fowler, C. C. Lauritsen, and T. Lauritsen, Phys. Rev. 106, 1260 (1957). 6 R. W. Peterson, W. A. Fowler, and C. C. Lauritsen, Phys. Rev. 96, 1250 (1954). T A B L E II. Cross section for the reaction He?{y,p)D. Total probable error including Experi- uncertainties in cr mental relative gamma-(MeV) (mb) error ray yields 6.14 (873-keV resonance) 0.109 9% 14% (935-keV resonance) 0.102 6% 7% 6.97 0.298 5% 16% 7.08 0.307 5% 8% The gamma flux was measured with an accurately calibrated N a l ( T h ) scinti l lat ion counter. The efficiency for this counter had been previously measured by Grif-fiths, Larson, and Rober tson 7 at a gamma-ray energy of 6.14 M e V . _ The photodisintegration spectra at the two fluorine resonances are shown in F i g . 1. Below 1.2 M e V , the spectra from the two resonances are essentially identical. I n calculating the cross sections at 6.92- and 7.12- M e V gamma-ray energies, no attempt was made to separate the peaks. Instead, the cross section is given in terms of a mean gamma-ray energy assuming the ratios of 6 . 9 2 -and 7.12-MeV gamma rays as given in Table I , and taking into account the rate of change of cross section wi th change i n gamma-ray energy. The experimental cross section values are shown in Table I I . The inverse reaction, D(\/>,7)He 3, has been studied by several worke r s . 7 - 1 1 Figure 2 shows the results of the application of the principle of detailed balance to the experimental measurements of Griffi ths. 1 1 The photo-disintegration cross-section values are shown for com-parison. The agreement is well wi th in experimental error. 7 G. M. Griffiths, E. A. Larson, and L. P. Robertson, Can. J. Phys. 40, 402 (1962). 8 W. A. Fowler, C. C. Lauritsen, and A. V. Tollerstrup, Phys. Rev. 76, 1767 (1949). 8 D. H. Wilkinson, Phil. Mag. 43, 659 (1952). 10 G. M. Griffiths and J. B. Warren, Proc. Phys. Soc. (London) A68, 781 (1955). 11 G. M. Griffiths (private communication). lM'l-'WWIA, if Reprinted from THE REVIEW OF SCIENTIFIC INSTRUMENTS, Vol . 33, No. 10, 1111-1112, October, 1962 Printed in U. S. A. Gas Flow Regulator for an rf Ion Source* B . L . WHITE, L . 1'. ROHERTSON,| K . L . ERDMAN, AND J . R. MACDONALDI Physics Department, University of British Columbia, Vancouver S, B. C, Canada (Received June 28, 1962) THE beam extracted from an ion source for injection into a Van de Graaff accelerator must be stable in intensity and focus for long periods of time. The intensity and focus are both functions of two externally controllable OSCILLATOR PLATE SUPPLY RF OSCILLATOR TO ACCELERATOR TUBE 1 A ION SOURCE OSCILLATOR COIL OAS FLOW REGULATOR i DIFFERENCE VR AMPLIFIER TO OAS BOTTLE FIG. 1. Block diagram of regulator system. ion source parameters, the plasma density and the ex-tracting field. Geometrical factors affecting the beam usually remain fixed while the ion source is operated, and the extracting field is easily regulated by conventional means. This leaves the plasma density as the factor whose stability will ultimately determine the beam stability. The plasma density is in turn a function of the power coupled into the discharge from the rf oscillator, and of the gas pressure within the discharge tube. However, > o o o e \u00a9 o o o o o\/o o o \u00a9\/o \u00a9 FIG. 2. Thermal leak. Body made of brass. The leak is mounted in an evacuated case for thermal stability and minimum power con-sumption. (1) Set screw, (2) soft solder vacuum seal, (3) Nichrome heater, 22.5 il, (4) stainless steel rod, (5) asbestos, (6) steel ball, (7) ball seat, taper formed with drill tip, ball forms tight shut-off seat by pressure deformation of brass. when the power supply voltages for the oscillator are set at fixed values, the power coupled into the plasma is directly proportional to the gas pressure in the discharge tube. This note describes an apparatus which stabilizes the plasma density by maintaining the oscillator power output constant at its optimum level by means of a servo system controlling the pressure in the discharge tube (Fig. 1). A signal proportional to the oscillator power regulates the flow of gas into the discharge tube. The gas flow rate is controlled by the power dissipation in the thermal leak heater (Fig. 2 ) . As the heater power is increased from zero, the leak temperature rises, and the differential expansion of the brass case and the stainless steel rod allows a gap to form between the ball and its seat, the size of the gap determining the leak rate from the high pressure reservoir into the discharge. The set screw is adjusted so that at a heater power input of 15 W the leak just begins to open; it will then shut off tight at OSCILLATOR PLATE SUPPLY FIG. 3. Servo circuit. a power input of about 6 W. In the present system, how-ever, the leak is not required to act as a tight shutoff, since the various gas supply bottles are shut off separately with solenoid valves. The servo circuit (Fig. 3) is driven by an error signal derived by comparing the voltage Vi .developed across Ri (by passing through Ri a fraction of the direct current in the rf oscillator plate circuit) to the reference voltage VJI developed across the Zener diodes D 3 and Di. The comparison is made in the difference amplifier Ti, after the dc level of V i has been shifted by means of the Zener diodes Di and D-.. The emitter-followers T\u00bb and T 3 provide successive stages of power gain. The gain feedback product around the loop (oscillator power level \u2014> difference am-plifier \u2014> power amplifier \u2014> thermal leak\u2014> gas pressure \u2014> oscillator power level) is about \u201410, which is sufficient to stabilize the discharge conditions so that the beam current onto the target of the accelerator is maintained constant to within a few percent over periods of many hours. * Research supported by a grant from Atomic Energy of Canada, Ltd. f Recipient of a National Research Council of Canada Studentship. APPENDIX G Rojirintcd from Tut: REVIEW OF SCIENTIFIC I N S T R U M E N T S , Vol. 34, No. 11, 1280-1281, November. 1963 Printed in U. S. A. Removal of Tritium from He 3* K. L. E R D M A N , \u2022 L. P. R O B E R T S O N , ! D . AxEN, f AND J. R . MACDONAI-Df Physics Department, University of British Columbia, Vancouver 8, B.C., Canada (Received 22 July 1963) CO M M E R C I A L L Y available H e 3 has a t r i t ium con-centration of approximately 2 parts in 10 s. As t r i t ium is beta active the concentration must be reduced to less than 1 part in 10 1 0 before H e 3 can be used in ionization chambers or proportional counters. Hanson et al.1 report concentrations of 7 parts in 10\" by dist i l l ing the H e 3 at 1\u00b0K. E l l i o t t 2 reports concentrations of 1 part in 10\" by absorbing the t r i t ium in pyrophoric uranium. We have found that similar concentrations are obtainable b y adding approximately 1% hydrogen to act as a carrier gas and then freezing the hydrogen and t r i t ium from the mixture at 4 .2\u00b0K. A schematic diagram of the purification system is shown i n F i g . 1. The helium cryostat was of standard design. The H e 3 was precooled in a l iquid nitrogen bath above the l iquid H e 4 . T w o German silver tubes 0.278 cm in diameter and 30 cm long, containing spiral inserts to increase the effective tube, length, were soldered together to serve as a heat exchanger. The trap in the cryostat had a volume of 6 cm 3 . The transfer pump was constructed of commercially available micro-finished Shelby steel tubing. The piston was fitted wi th a double O-ring seal and the port ion of the upper cylinder below the piston was connected to a reser-voir filled wi th argon such that the argon pressure always exceeded the H e 3 pressure above the piston. This pre-caution insured that no nitrogen or oxygen would con-taminate the H e 3 and destroy its qual i ty as a counter gas. The piston was driven by compressed air admitted to the lower of the two cylinders. The purification procedure was as follows. The system TO GEIOER COUNTER 6 SYSTEM F I G . 1. Schematic of He* pur-ification system. TO AIR CONTROL FOR TRANSFER PUMP DRIVE HELIUM CRYOSTAT 2 N OTES \u2022was evacuated and tested for leaks. The cryostat was cooled to liquid helium temperature with the vacuum system connected to ensure that no leaks developed during the cooling process. Carrier hydrogen was then added to the impure He 3. With the valve to the transfer pump closed, the gas from the bottle was leaked slowly into the trap in the cryostat until the pressure in the system came to equilibrium. This usually took 2 to 3 min. The initial pressure in the He 3 bottle was slightly below atmospheric pressure. The valve to the bottle was closed and the gas in the trap was transferred to the clean storage bottle using the transfer pump. The process was repeated until the He 3 bottle was evacuated. During the purification, samples of the purified gas were let into a Geiger counter of 25-cm3 active volume and the activity.measured. With 1900 V applied to the central electrode of the counter, a Geiger plateau of 150 V was achieved with a filling of 2.5 cm Hg of helium and 10 cm Hg of methane. The counting was done with a Berkeley scaler model 2001. The background activity was measured with a He4-methane mixture. The counter had to be etched after a few runs to remove the background due to tritium occluded at the walls. 6.5 liters of He 3 were purchased from the Monsanto Corporation with a quoted tritium concentration of 1.7 parts in 108. With the addition of 1% hydrogen to the He 3, the tritium concentration was reduced to 6 \u00b1 2 parts in 10\". Approximately 2.5 liters of liquid helium were evaporated in the process. * Research supported by a grant from Atomic Energy of Canada Ltd. t Recipient of a National Research Council of Canada Studentship, 1961-63. 1 E. R. Hanson, H. H. Otuski, L. Passell, W. H. Lien, and N. E. Phillips, Rev. Sci. Instr. 30, 591 (1959). 2 M. J. W. Elliott, Rev. Sci. Instr. 31, 1218 (1960). APPENDIX H Reprinted from T H E REVIEW OE SCIENTIFIC I N S T R U M E N T S , Vol. 35, No. 2, 241, February 1964 Printed in U. S. A. Simple Gas Circulation Pump* K . L . E R D M A N , J. R . M A C D O N A L D , ! G . A . BEER,*; 'AND D . A . A X E N | Physics Department, University of British Columbia, Vancouver 8, British Columbia, Canada (Received 10 October 1963) ' | V H E standard method of purifying gases in ionization chambers, proportional counters, and gas scintilla-tion counters is to pass the gas over hot calcium-magnesium eutectic mixtures.1'2 One usually depends on convection currents to circulate the gas through the purifier. For efficient circulation of the gas, the tubes leading to and from the purifier must be large, and thus the volume of purifier and associated connections may represent a large fraction of the total volume of the chamber. This note describes a pump with a small volume and relatively high rate of gas circulation. The details of construction of the pump are shown in Fig. 1. The cycle is as follows: (1) -The piston is shown in the position with the solenoid energized. The solenoid is energized by a pulse of 0.3-sec duration that drives the piston upwards. During this part of the cycle the upper valve is closed, pushing the gas out of the pump cylinder, and the lower valve opens to admit gas to the lower part of the pump cylinder. (2) When the voltage pulse is removed from the solenoid, the piston falls under gravity and is stopped by the spring. The lower valve closes and the upper valve opens, allowing the gas to leak into the space above the piston. The piston clearance in the cylinder is 0.002 in. and negligible leakage occurs during the stroke. The cycle is repeated once per second. The total dis-placement of gas per cycle is 4 cm 3 for the size pump shown. One can thus pump 14 liters\/h. The pump may be operated continuously for several months without excessive wear or loss of efficiency and has been tested at pressures up to 11 atm. * Research supported by a grant .from Atomic Energy of Canada, Ltd. t Recipient of a National Research Council of Canada Studentship (1961-1963). X Present Address: University of Saskatchewan, Saskatoon, Saskatchewan, Canada. ' O. Ruff and H. Hartmann, Z. Anorg. Allgem. Chem. 121, 167 (1922). 2 N. Colli and U . Facchini, Rev. Sci. Instr. 23, 39 (1952). SCALE - INCHES FIG. 1. Gas circulation pump. All joims are silver soldered. (1) copper tube; (2) adjustable clamp to hold solenoid; (3) soft iron cap, slotted for removal; (4) mild steel valve; (5) soft iron piston; (6) ac or dc solenoid; (7) stainless steel cylinder; (8) piano wire spring; (9) screw cap, slotted; (10) 3 equally spaced ports; (11) Neoprene O-ring; (12) 6 equally spaced screws; (13) mild steel valve; and (14) copper tube. APPENDIX I Reprinted from T H K RKVIKW OK SCIENTIFIC INSTRUMENTS, Vol. 35, No. 1, 122-123, January 1964 rrintcd in U. S. A. Simple Electron Bombardment Apparatus for Evaporating Boron* K . L . E R O M A N , D . A X E N,! J. R. M A C D O N A L D , ! AND L . P . R O B E R T S O N ! Physics Department, University of British Columbia, Vancouver S, B. C, Canada (Received 22 July 1963; and in final form, September 16, 1963) ' | % HIS note describes an electron bombardment appara-tus which has proven to be successful in preparing evaporated films of high resistivity materials. Tempera-tures in excess of 2500\u00b0C were obtained. The evaporator (Fig. 1) was enclosed in a commercially available1 2-in. Pyrex tee connection (1). This design has the advantages that no high voltage vacuum feedthrough and no water-cooling connections are required. The filament power was supplied by a 115-A 5-V trans-former. The high voltage was supplied by a Scientific Electric model P3-238 dc power supply rated to deliver FIG. 1. Schematic vertical section of electron bombardment apparatus. 20 mA current at 20 kV. The glass tee was cooled with a Dayton model 2C 610 air blower. The evaporator was attached to a mercury diffusion pump which produced a residual pressure of approximately 2 X IO - 5 mm Hg. Two threaded brass rods served as filament terminals. One of the rods (2) was attached to the brass plate (3) at the top of the glass tee. The other (4) was admitted through a Kovar seal (5). The upper brass plate was at ground potential. Two 0.010-in.-thick tantalum plates \\ in. apart, (6), served as focusing electrodes for the electron beam. The hole through the center of these plates was XTT in. in diameter. The filament (7) consisted of a single turn of O.OlO-in.-diam tungsten wire 2 in. long. The material to be evaporated was placed in a well at the top of a carbon rod (8) \\ in. in diameter and \\ \\ in. long. For the reasons dis-cussed by H i l l , 2 the carbon rod was attached to a brass Sylphon bellows (9) movable in all three directions by the adjusting screw (10). The metal backing (11), onto which the film was deposited, was clamped to the grounded filament electrode approximately l^ - in. above the upper tantalum plate. The high voltage lead was connected directly onto the brass plate (12) at the lower end of the glass tec. Initially, the carbon rod was outgassed by applying 5 k V to the lower plate and enough filament current to produce approximately 1 mA of electron current and then pumping the system for \\ h. A typical set of operating conditions during the evaporation of boron, which requires tempera-tures above 2500\u00b0C, was filament current, 6A; accelerating voltage, 5 k V ; electron current, .20-30 m A ; and pressure, 4 X l f r s nun Hg. The apparatus was operated under these conditions for periods up to 3 h. Under these conditions red diffraction rings appeared on the film at a rate of one per minute. This rate of deposition was extremely sensitive to the position of the boron. The best results were obtained when the boron was situated approximately ^ in.'below the lower tantalum plate. < * Research supported by a grant from Atomic Energy of Canada Ltd. ! Recipient of a National Research Council of Canada Studentship 1961-63. 1 Pyrex tec available from Corning Glass Works, Corning, New \u2022\u2022'-Sifork.' 2 H. A. Hill, Rev. Sci. fnstr. 27, 10S6 (1956). APPENDIX J Charged Photoparticles from Argon M.A. Reiraann, J.R. MacDonald and J.B. Warren Abstract 4 0 j. Charged photoparticles from A have been observed i n a gridded i o n i z a t i o n chamber i r r a d i a t e d with 9.17 MeV and 17.71 MeV gamma rays. P a r t i a l and t o t a l cross sections are given for the reactions 4 0 A ( r , p ) 3 9 C l and 4 oA ( j<,a ) 3 6 S . I. Introduction Because i t i s r e l a t i v e l y well understood, the electromagnetic i n t e r a c t i o n suggests i t s e l f as a powerful t o o l for the investigation of nuclear structure. Thus quanta of r a d i a t i o n have the advantage over p a r t i c l e s as participants i n nuclear reactions, i n that the i n t e r a c t i o n Hamiltonian i s known. Over the past two decades t h i s know-ledge has been u t i l i z e d i n the construction of nuclear models enjoying considerable success i n accounting f o r the giant dipole absorption resonance observed i n nuclear reactions . The advance of our understanding of the mechanism involved i n photonuclear d i s i n t e g r a t i o n following the large amount of experimental work which has been done^ , has been hampered by the lack of a suitable source of gamma rad i a t i o n , and shortcomings i n instrumentation f o r monitoring the a v a i l a b l e sources. Bremsstrahlen have been used e f f e c t i v e l y to e s t a b l i s h the shape of the dipole resonance, and to reveal the gross features of the energy d i s t r i b u t i o n of the photo-di s i n t e g r a t i o n products. The r e s u l t s have been used to estimate l e v e l densities i n heavier n u c l e i , and have lead to descriptions of the d i s i n t e g r a t i o n process i n terms of both s t a t i s t i c a l 6 ^ and d i r e c t photoeffect 7^ models. In order to assess the pertinence of these models, and i n order to examine the f i n e structure, both of the dipole absorption cross section as a function of energy and of the energy spectrum of emitted photoparticles, the photodisintegration must be i n i t i a t e d by a monochromatic source. To t h i s end the photodisintegration of argon at 17.6 MeV e x c i t a t i o n was investigated by Wilkinson and 8) Carver 9 ] Our present knowledge of the reaction Q-values ', as pointed out by S p i c e r * 0 ^ , does hot admit the i n t e r -pretation placed by Wilkinson and Carver upon t h e i r r e s u l t s . For t h i s reason the reactions 4 0 A ( ^ , p ) 3 9 C l and 4 o A ( ^ , a ) 3 6 S have been re-examined at a photon energy Of 17.71 MeV and the cross sections determined. In addition the photoalpha cross section was measured at a photon energy of 9.17 MeV. 2 . E x p e r i m e n t a l The e n e r g y s p e c t r a o f c h a r g e d p h o t o p a r t i c l e s were o b t a i n e d u s i n g a g r i d d e d i o n i z a t i o n c h a m b e r . The chamber i s d e s c r i b e d by Hay a n d W a r r e n 1 1 \\ b u t i n t h e p r e s e n t c a s e t h e i n t e r i o r was l i n e d w i t h a 35 um t h i c k n e s s o f M y l a r w i t h s u f f i c i e n t g o l d e v a p o r a t e d o n t o i t t o r e d u c e t h e r e s i s t i v i t y o f t h e i n n e r s u r f a c e t o a p p r o x i m a t e l y a t h o u s a n d ohms p e r cm. T h i s t e c h n i q u e was f o u n d more e f f e c t i v e t h a n a g r a p h i t e c o a t i n g f o r r e d u c i n g b a c k g r o u n d due t o a c t i v i t y i n t h e chamber w a l l s . The chamber was f i l l e d w i t h h i g h g r a d e w e l d i n g a r g o n c o n t a i n i n g l e s s t h a n 0 . 0 2 % o f i m p u r i t i e s , t h e s e b e i n g o x y g e n , n i t r o g e n , h y d r o g e n and c a r b o n d i o x i d e . A f t e r f i l l i n g , t h e i m p u r i t y c o n t e n t was f u r t h e r r e d u c e d by c o n v e c t i o n c i r c u l a t i o n o f t h e gas t h r o u g h a h e a t e d s i d e a r m c o n t a i n i n g a c a l c i u m - m a g n e s i u m ' 12) \"\" '\" e u t e c t i c m i x t u r e W i t h an a r g o n p r e s s u r e o f 6 . 8 0 atm a few h o u r s o f p u r i f i c a t i o n i n t h i s manner r e s u l t e d i n an e n e r g y r e s o l u t i o n o f 4% f o r 5 . 1 5 MeV a l p h a p a r t i c l e s f r o m a Pu239 c a l i b r a t i n g s o u r c e . The c a l c i u m - m a g n e s i u m e u t e c t i c c o n t a i n e d r a d i o a c t i v e 222 i m p u r i t i e s w h i c h e m i t t e d t h e i s o t o p e Rn . T h i s i s o t o p e was i d e n t i f i e d f r o m t h e ; p e a k s p r o d u c e d i n t h e chamber b a c k -g r o u n d c o r r e s p o n d i n g t o t h e e n e r g i e s p r e d i c t e d by t h e d e c a y scheme f o r t h i s n u c l e i d e . W h i l e t h e s e p e a k s i n t u r n p r o v i d e d a u s e f u l c h e c k on t h e e n e r g y s c a l e s e t by t h e c a l i b r a t i n g s o u r c e , t h e b a c k g r o u n d a c t i v i t y c o u l d be r e d u c e d t o n e g l i g i b l e p r o p o r t i o n s f o r t h e d u r a t i o n o f t h e e x p e r i m e n t a l work by b e g i n n i n g t h e r u n s w i t h i n a few h o u r s o f f i l l i n g t h e chamber w i t h f r e s h g a s . V o l t a g e p u l s e s f r o m t h e chamber were a m p l i f i e d by a D y n a t r o n P r e a m p l i f i e r U n i t m o d i f i e d t o i n c o r p o r a t e a t y p e 7586 N u v i s t o r a s a f i r s t s t a g e , f o l l o w e d by a D y n a t r o n M a i n A m p l i f i e r 1430 A . D i f f e r e n t i a t i n g a n d i n t e g r a t i n g t i m e c o n s t a n t s o f 8 u s were u s e d f o r p u l s e s h a p i n g , a n d p u l s e s were a n a l y s e d i n 128 c h a n n e l s o f a N u c l e a r D a t a M o d e l ND 103 256 c h a n n e l p u l s e h e i g h t a n a l y s e r . Gamma f l u x measurements were made w i t h a 6 . 9 8 cm d i a m e t e r by 1 1 . 4 cm l o n g N a l ( T l ) c r y s t a l . The e f f i c i e n c y o f t h i s s c i n t i l l a t i o n c o u n t e r has been d e t e r m i n e d t o w i t h i n 15% a t 1 7 . 7 MeV, a n d i s known t o w i t h i n 10% a t 9 . 1 7 M e V 1 3 - 1 5 ) . The gamma s p e c t r a were a l s o m o n i t o r e d b y a N u c l e a r D a t a M o d e l ND 120 256 c h a n n e l p u l s e h e i g h t a n a l y s e r . The 9 . 1 7 MeV gamma r a y s were o b t a i n e d by b o m b a r d i n g a 1 3 C t a r g e t 3 0 keV t h i c k w i t h 1 .75 MeV p r o t o n s f r o m t h e U n i v e r s i t y o f B r i t i s h C o l u m b i a 3 MeV Van de G r a a f f a c c e l e r a t o r . The t a r g e t was p r e p a r e d b y c r a c k i n g i s o t o p i c a l l y e n r i c h e d m e t h y l i o d i d e o n t o a p l a t i n u m b a c k i n g 1 6 K The y i e l d o f 9 . 1 7 MeV gamma r a y s was d e t e r m i n e d by s p e c t r u m s t r i p p i n g t o s e p a r a t e o u t t h e 6 . 4 4 MeV c o m p o n e n t 1 6 ) . F o r t h e 9 . 1 7 MeV w o r k , t h e i o n i z a t i o n chamber was s i t u a t e d a t 90\u00b0 t o t h e p r o t o n beam. Gamma r a y s o f e n e r g y 1 7 . 6 4 MeV were o b t a i n e d f r o m t h e r e a c t i o n ^ L i C p , ? ' ) ^ e a t t h e 441 keV r e s o n a n c e . A d i f f e r e n t t a r g e t was u s e d f o r e a c h r u n , t h e s e b e i n g p r o d u c e d by e v a p o r a t i n g m e t a l l i c l i t h i u m o n t o a c o p p e r b a c k i n g . The t a r g e t t h i c k n e s s v a r i e d f r o m 3 0 KeV t o 60 k e V . The i o n i z a t i o n chamber was a t 0\u00b0 t o t h e p r o t o n beam. A t t h i s p o s i t i o n t h e D o p p l e r s h i f t i s + 67 k e V , g i v i n g p h o t o n s o f e n e r g y 1 7 . 7 1 MeV. x The r a t i o o f 1 7 . 7 MeV t o 1 4 . 8 MeV gamma r a y s was o b t a i n e d by s p e c t r u m s t r i p p i n g . F o r t h i s p u r p o s e t h e s p e c t r a l s h a p e o f t h e 1 7 . 7 MeV component was assumed t o be s i m i l a r t o t h a t o f t h e 1 7 . 1 MeV component f r o m t h e r e a c t i o n ^B(p,y)^C a t a b o m b a r d i n g e n e r g y o f 1 .2 MeV. A t t h e s c i n t i l l a t i o n c o u n t e r , p o s i t i o n e d a t 138\u00b0 t o t h e p r o t o n beam, t h e r a t i o o f 1 7 . 6 t o 1 4 . 8 MeV gamma y i e l d s was f o u n d t o v a r y f r o m 1 , 8 7 +_ 0 . 1 f o r a 3 0 keV t a r g e t t o 1 . 7 8 + 0 . 1 f o r a 60 keV t a r g e t . T h e s e r e s u l t s a r e c o n s i s t a n t w i t h t h o s e o b t a i n e d by M a i n s b r i d g e i 7 ) . The r a t i o o f y i e l d s i n c r e a s e s by a p p r o x i m a t e l y 4% when o b s e r v e d a t 0\u00b0 t o t h e p r o t o n beam, due t o t h e a n i s o t r o p i e s i n v o l v e d 1 \u00ae ) . The gamma f l u x t h r o u g h t h e chamber was c a l c u l a t e d a c c o r d i n g l y . 3 . R e s u l t s A c a l c u l a t i o n o f t h e c r o s s s e c t i o n f o r t h e e v e n t s o b s e r v e d r e q u i r e s k n o w l e d g e o f t h e e f f i c i e n c y o f t h e i o n i z a t i o n c h a m b e r . T h i s i s a g e o m e t r i c c a l c u l a t i o n c o m p r i s i n g i n t e g r a t i o n over the s e n s i t i v e volume of the chamber to e s t a b l i s h the mean gamma f l u x - p a t h l e n g t h product. This c a l c u l a t i o n was 19) c a r r i e d out by Axen and Robertson ' a s a f u n c t i o n of chamber dimensions and t a r g e t p o s i t i o n . The number of events a s s o c i a t e d w i t h each peak i d e n t i f i e d i n the p h o t o p a r t i c l e energy d i s t r i b u t i o n s was obtained by c o r r e c t i n g the number of counts i n the peak f o r time dependent background, w a l l e f f e c t and, i n the 17.7 MeV work, estimated c o n t r i b u t i o n due to 14.8 MeV r a d i a t i o n . Wall e f f e c t i s due t o two causes, and r e s u l t s i n the accumulation of counts i n the s p e c t r a a t energies lower than a c t u a l l y a s s o c i a t e d w i t h the charged p a r t i c l e s causing them. The most important c o n t r i b u t i o n to w a l l e f f e c t i s the w a l l l o s s . T h i s r e s u l t s i f the charged p a r t i c l e s o r i g i n a t i n g from a p h o t o d i s i n t e g r a t i o n event do not l o s e a l l t h e i r energy by i o n i z a t i o n of the gas i n the s e n s i t i v e volume of the chamber, e i t h e r because of c o l l i s i o n w i t h the chamber w a l l or because they leave the s e n s i t i v e volume and proceed i n t o the dead spaces at the ends of the chamber. The other c o n t r i b u t i o n t o w a l l e f f e c t i s the end e f f e c t . This r e f e r s t o events t a k i n g place i n the dead spaces g i v i n g r i s e t o charged p a r t i c l e s which enter the s e n s i t i v e volume a f t e r l o s i n g some of t h e i r energy ou t s i d e i t . The c a l c u l a t i o n of the w a l l e f f e c t i s a l s o a geometric one, i n v o l v i n g the chamber dimensions and the p a r t i c l e ranges, and has been treated i n d e t a i l for c y l i n d r i c a l chambers by Robertson 1 9). The necessary corrections to the cross sections varied from 41% for the most energetic protons to 6% for the lea s t energetic alphas. The predominating source of uncertainty i n our values for the cross sections i s the gamma spectrometer e f f i c i e n c y . The experimental uncertainties i f the gamma counter e f f i c i e n c y were known exactly, are also indicated with the experimental r e s u l t s i n table 1. A considerable uncertainty, +_ 15% for the 9.17 MeV r e s u l t s , i s due to the r e l a t i v e l y large background subtraction involved. This uncertainty i s smaller for the 17.71 MeV work. Other sources of uncertainty, such as knowledge of the angular d i s t r i b u t i o n s of the gamma rays, have been considered i n estimating the possible error of our r e s u l t s , but these are much smaller than the two already mentioned and w i l l not be discussed further. 3.1 Results at 9.17 MeV The energy d i s t r i b u t i o n of charged photoparticles from argon i r r a d i a t e d with 9.17 MeV gamma rays i s shown i n f i g . 1. We i d e n t i f y the peak at 2.29 MeV with the reaction 40 *3fi A(y,a) S leaving the re s i d u a l nucleus i n i t s ground state. We obtain a Q-value of =6.88 + 0.1 MeV for t h i s reaction, i n 9) agreement with Everling ejt aJL , who obtain -6.81 +_ 0.01 MeV. The t o t a l c r o s s s e c t i o n f o r t h e r e a c t i o n i s 31 +_ 6 u b . 3 . 2 R e s u l t s a t 1 7 . 7 1 MeV The i r r a d i a t i o n w i t h l i t h i u m gamma r a y s gave t h e c h a r g e d p h o t o p a r t i c l e s p e c t r a shown i n f i g . 2 . F i g . 2 ( a ) c o m p r i s e s s p e c t r a o b t a i n e d w i t h 6 . 8 0 atm a n d 3 . 4 0 atm o f a r g o n p r e s s u r e r e s p e c t i v e l y , a n d f i g . 2 ( b ) shows r e s u l t s o b t a i n e d a t 7 . 0 1 atm w i t h i m p r o v e d e n e r g y r e s o l u t i o n . The i d e n t i f i c a t i o n o f p e a k s B a n d C a s p h o t o a l p h a p e a k s i s c o n f i r m e d by c o m p a r i s o n o f t h e s p e c t r a i n f i g . 2 ( a ) . B o t h g i v e t h e same c r o s s s e c t i o n w i t h i n e x p e r i m e n t a l e r r o r when w a l l e f f e c t c o r r e c t i o n s a p p r o p r i a t e t o a l p h a p a r t i c l e s a r e made f o r p e a k s B a n d C , a n d a p p r o p r i a t e t o p r o t o n s a r e made f o r peak D . D i f f e r e n t a s s i g n m e n t s w o u l d n o t g i v e s u c h a g r e e m e n t . B e c a u s e o f t h e w i d t h o f t h e 1 4 . 8 MeV component o f t h e gamma f l u x , i t s c o n t r i b u t i o n t o t h e p h o t o p a r t i c l e s p e c t r u m i s d i s t r i b u t e d o v e r a l a r g e e n e r g y i n t e r v a l a n d hence d o e s n o t i n f l u e n c e t h e s t r u c t u r e s i g n i f i c a n t l y . 2 0 ) F u r t h e r m o r e , t h e b r e m s s t r a h l u n g work o f M c P h e r s o n e t a l shows t h e 4 0 A ( y , p ) 3 9 C l c r o s s s e c t i o n a t 15 MeV t o be down b y a f a c t o r o f s i x f r o m t h a t a t 18 MeV. We assume t h a t t h i s r e d u c t i o n i n t h e c r o s s s e c t i o n i s e n t i r e l y due t o t h e shape o f t h e d i p o l e r e s o n a n c e , s o we u s e t h e same f a c t o r i n c o m p u t i n g t h e y i e l d o f p h o t o a l p h a s due t o t h e 1 4 . 8 MeV r a d i a t i o n from that measured at 17.71 MeV. Thus the number of counts due to the 14.8 MeV gammas was estimated for each possible reaction by taking the number of counts due to the 17.71 MeV gammas for the same reaction corrected for background but not wall e f f e c t , reducing i t by the McPherson et a l factor of s i x , and further reducing i t i n proportion to the r a t i o of 14.8 to 17.71 MeV gamma rays. For the purpose of subtraction from the charged p a r t i c l e spectrum, the approximation was made that these counts were evenly d i s t r i b u t e d over a 2 MeV i n t e r v a l centred on the appropriate energy. In no case did t h i s correction exceed 5%. The r e s u l t s at 17.71 MeV are summarized i n table 1. 4. Discussion If the photonuclear process i n argon proceeds l a r g e l y through the formation of a compound nucleus, the r a t i o of p a r t i a l cross sections f o r decay by charged p a r t i c l e emission through various channels should simply be that of the respective p e n e t r a b i l i t i e s . It would there-fore be expected that the p a r t i a l cross section for 40 39 A(JSP) c l t o t h e ground state of \u00b09C1 would be larger than that to i n d i v i d u a l excited states. We therefore suppose that the peak \u00a3 of f i g . 2 represents t r a n s i t i o n s t o more t h a n one e x c i t e d s t a t e o f C l n o t r e s o l v e d i n our e n e r g y d i s t r i b u t i o n . T h i s p o s s i b i l i t y i s s u p p o r t e d by E n d t a n d v a n d e r L e u n 2 * ^ who show l e v e l s i n ^ 9 C 1 a t 0 . 3 6 and 0 . 8 MeV. On t h e o t h e r h a n d , t h e s u p p o s i t i o n t h a t peak E r e p r e s e n t s two o r more l e v e l s i n ^ C l makes t h e p a r t i a l c r o s s s e c t i o n f o r t h e g r o u n d s t a t e t r a n s i t i o n a p p e a r l a r g e r t h a n p r e d i c t e d f r o m s t a t i s t i c a l c o n s i d e r a t i o n s ; l a r g e r by an e x t e n t d e p e n d e n t u p o n t h e s p i n and p a r i t y a s s i g n m e n t s f o r t h e e x c i t e d s t a t e s , a n d d e p e n d e n t upon how much l o w e r t h a n c l a s s i c a l t h e Coulomb b a r r i e r h e i g h t i s due t o f u z z i n e s s o f t h e n u c l e a r s u r f a c e 2 2 S i n c e t h e p r e d i c t i o n s o f t h e r a t i o o f p e n e t r a b i l i t i e s c a n o n l y be c o n s i d e r e d as a p p r o x i m a t e , i t i s n o t p o s s i b l e t o e s t i m a t e t o what e x t e n t t h i s p a r t i a l c r o s s s e c t i o n r a t i o h a s been i n f l u e n c e d b y c o n t r i b u t i o n s f r o m a d i r e c t p h o t o -e f f e c t . The r a t i o o f t h e p a r t i a l c r o s s s e c t i o n t o t h e g r o u n d 36 s t a t e o f S by a l p h a e m i s s i o n a n d t o t h e g r o u n d s t a t e o f 39 C l b y p r o t o n e m i s s i o n a t 17.71 MeV e x c i t a t i o n was o b s e r v e d t o be a n o r d e r o f m a g n i t u d e s m a l l e r t h a n p r e d i c t e d f r o m t h e p e n e t r a b i l i t i e s . T h i s m i g h t i n p a r t be due t o a s m a l l f o r m a t i o n f a c t o r 2 3 ) f o r a l p h a p a r t i c l e s i n t h e compound n u c l e u s , b u t t h i s c o u l d n o t a c c o u n t f o r t h e e n t i r e d i s -c r e p a n c y . I n t h e a b s e n c e o f known s e l e c t i o n r u l e s o p e r a t i n g 36 a g a i n s t t h e a l p h a t r a n s i t i o n t o t h e g r o u n d s t a t e o f S , t h e e x i s t e n c e o f a n o t h e r l o w l y i n g l e v e l i n ^Cl c o n t r i b u t i n g t o peak D o f f i g . 2 may be i n d i c a t e d . A l t e r n a t i v e l y , t h e c r o s s s e c t i o n f o r a l p h a e m i s s i o n t o t h e g r o u n d s t a t e o f 3 6 S may have b e e n o b s e r v e d a t an e x c u r s i o n b e l o w i t s a v e r a g e v a l u e , d e m o n s t r a t i n g t h e e x i s t a n c e o f e x c i t a t i o n e n e r g y d e p e n d e n t c r o s s s e c t i o n f l u c t u a t i o n s a s d e s c r i b e d b y E r i c s o n 2 4 * 2 5 ) . We a r e i n d e b t e d t o t h e N a t i o n a l R e s e a r c h C o u n c i l o f Canada f o r f i n a n c i a l s u p p o r t a n d f o r a w a r d i n g s t u d e n t -s h i p s t o two o f u s ( M . A . R . a n d J . R . M . ) . We w i s h t o t h a n k D r . E . V o g t f o r h i s most h e l p f u l comments , a n d M r . E . W . B l a c k m o r e f o r r e p r o g r a m m i n g t h e gamma f l u x - p a t h l e n g t h c a l c u l a t i o n s f o r t h e i o n i z a t i o n c h a m b e r . Figure 1 Figure 2(a) Figure 2(b) Table 1 Experimental r e s u l t s at 17.71 MeV Spectrum peak Reaction A 4 0 A ( r , a ) 3 6 S Remarks To ground state of 36, Q-value MeV - 6.6+0.4 Cross section mb 0.08+0.05 B 4 0 A ( r , a ) 3 6 S To excited state(s) of 36s at e& 3.5 MeV -10.1+0.1 0.35+0.06 4\u00b0A( r,\u00ab)36 S To excited state(s) of ,36s at 4.7 MeV -11.3+0.1 0.40+0.08 40., ,36c A(^,a) S Total cross section 0.83+0.16 (+ 0\".09) D 4 0 A ( r , p ) 3 9 C l oq To ground state of C l -12.46+0.1 1.15+0.2 E 4 0 A ( r , p ) 3 9 C 1 39 To excited states of C l at 0.5 MeV -12.99+0.1 1.26+0.2 F,G 4 0 A ( r , p ) 3 9 C l To excited states of 3 9 C 1 4.75+1.0 4 0 A ( r , P ) 3 9 C l Total cross section 7.16+1.26 (+0.5*6) The uncertainties i n brackets are estimated on the assumption that the e f f i c i e n c y of the gamma counter i s known exactly. FIGURE CAPTIONS F i g . 1: The photodisintegration of 4 0 A at 9.17 MeV showing the photoalpha peak. 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Barnes, CA,, Carver, J.H,, and Stafford, G.H. (1952), Phys. Rev, 86, 359. Wilkinson, D.H, and Bloom, S.D. (1957), P h i l . Mag. 2, 63. Woodbury, H.H., Day, R.B., and Tollestrup, A.V. (1953), Phys. Rev. 92, 1199. ","attrs":{"lang":"en","ns":"http:\/\/www.w3.org\/2009\/08\/skos-reference\/skos.html#note","classmap":"oc:AnnotationContainer"},"iri":"http:\/\/www.w3.org\/2009\/08\/skos-reference\/skos.html#note","explain":"Simple Knowledge Organisation System; Notes are used to provide information relating to SKOS concepts. 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