/* 2005-12-19 File is generated by HENDEL. */ \\BIB,1[69; D#=D1523; TITLE=/ Hole strengths and spreading widths observed in 92Mo(p,d)91Mo reaction at 65 MeV /; PURPOSE=/ To assign spin-parities and determine spectroscopic factors of excited neutron-hole states of 91Mo nuclei in the excitation energy region of 0-10 MeV /; ATH=(K.HISAMOCHI'1', O.IWAMOTO'1', A.KISANUKI'1', S.BUDIHARDJO'1', S.WIDODO'1', A.NOHTOMI'1', Y.UOZUMI'1', T.SAKAE'1', M.MATOBA'1', M.NAKANO'2', T.MAKI'2', S.MATSUKI'3', N.KOORI'4'); INST-ATH=(2JPNKYU'1', 2JPNKIT'2', 2JPNKTO'3', 2JPNTKS'4'); /* '1' Faculty of Engineering */ /* '2' School of Nursing and Technology */ /* '3' Chemical Research Institute */ /* '4' College of General Education */ REF=NP/A; VLP=564(1993)227; RCTS=92MO(P,D)91MO; PHQS=(ANGL-DSTRN, VCTR-ANALPW, SPEC-FCTR); \\EXP,1[69; /* 2005-10-12 : Converted, Kc + Sr + On. Converted to EXFOR E523 */ /* 2005-11-12 : Altered, On + Kc + Sr. Re-digitized */ ENR=X%'5'; /* '5' Enriched target */ CHM=ELM; PHYS-FORM=SLD; THK-TGT=0.506MG/CM**2; POL-TGT=0%; ALGN-TGT=0%; ACC=CYC'6'; /* '6' Isochronous cyclotron, AVF cyclotron */ INST-ACC=2JPNRCN; INC-ENGY-LAB=65MEV; POL-PRJ=X%'7'; /* '7' A polarized proton beam was used */ DET-PARTCL=D; COINC=NO; ANT-COINC=NO; DET-SYS=MAG'8'; /* '8' Spectrograph RAIDEN [H. Ikegami et al., Nucl. Instr. Meth. 175(1980)33] viewed with the focal plane detector system KYUSHU [M. Matoba et al., Nucl. Instr. Meth. 180(1980)419] */ ERS-DET=40KEV; ANL=DWBA; \\EXP,1; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,1; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'9',X%'10'); /* '9' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '10' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=0.000MEV; J-PTY=9/2+; TRNSF-L=4'11'; /* '11' Transferred orbital angular momentum (L) */ TRNSF-J=9/2'12'; /* '12' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.568E+00 6.994E+00 +-3.035E-01 7.643E+00 5.590E+00 +-1.454E-01 1.067E+01 4.702E+00 +-1.424E-01 1.388E+01 4.454E+00 +-1.119E-01 1.682E+01 4.421E+00 +-1.109E-01 1.989E+01 3.997E+00 +-1.004E-01 2.311E+01 3.075E+00 +-7.723E-02 2.600E+01 2.137E+00 +-5.367E-02 2.921E+01 1.700E+00 +-4.271E-02 3.238E+01 1.638E+00 +-4.100E-02 3.532E+01 1.408E+00 +-NEGLIGIBLE 4.060E+01 9.077E-01 +-2.280E-02 4.565E+01 6.267E-01 +-1.314E-02 \END; /* Data scanned from left hand side of Fig.2a, p231 in reference */ \\EXP,2; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,2; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'13',X%'14'); /* '13' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '14' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=1.902MEV; J-PTY=9/2+; TRNSF-L=4'15'; /* '15' Transferred orbital angular momentum (L) */ TRNSF-J=9/2'16'; /* '16' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.624E+00 3.358E-01 +-4.538E-02 7.426E+00 3.939E-01 +-2.831E-02 1.050E+01 3.941E-01 +-3.178E-02 1.375E+01 4.056E-01 +-3.271E-02 1.666E+01 3.945E-01 +-2.320E-02 1.988E+01 3.435E-01 +-2.169E-02 2.284E+01 2.712E-01 +-1.015E-02 2.595E+01 1.656E-01 +-9.025E-03 2.916E+01 1.367E-01 +-1.103E-02 3.207E+01 1.303E-01 +-8.227E-03 3.520E+01 1.125E-01 +-6.133E-03 4.064E+01 7.650E-02 +-6.169E-03 4.570E+01 4.934E-02 +-3.979E-03 \END; /* Data scanned from left hand side of Fig.2a, p231 in reference */ \\EXP,3; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,3; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'17',X%'18'); /* '17' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '18' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=2.226MEV; J-PTY=9/2+; TRNSF-L=4'19'; /* '19' Transferred orbital angular momentum (L) */ TRNSF-J=9/2'20'; /* '20' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.742E+00 5.431E-02 +-1.770E-02 7.636E+00 4.570E-02 +-9.300E-03 1.076E+01 4.629E-02 +-1.036E-02 1.387E+01 6.732E-02 +-8.741E-03 1.681E+01 5.737E-02 +-7.722E-03 1.998E+01 5.363E-02 +-6.964E-03 2.278E+01 3.995E-02 +-5.377E-03 2.604E+01 2.578E-02 +-3.103E-03 2.916E+01 1.773E-02 +-2.988E-03 3.210E+01 1.773E-02 +-2.217E-03 3.526E+01 1.623E-02 +-2.418E-03 4.060E+01 1.255E-02 +-1.810E-03 4.562E+01 8.594E-03 +-1.364E-03 \END; /* Data scanned from left hand side of Fig.2a, p231 in reference */ \\EXP,4; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,4; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'21',X%'22'); /* '21' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '22' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=2.454MEV; J-PTY=9/2+; TRNSF-L=4'23'; /* '23' Transferred orbital angular momentum (L) */ TRNSF-J=9/2'24'; /* '24' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.847E+00 4.974E-01 +-1.535E-01 7.597E+00 6.479E-01 +-1.381E-01 1.071E+01 8.262E-01 +-1.189E-01 1.392E+01 7.465E-01 +-1.219E-01 1.681E+01 7.556E-01 +-8.370E-02 1.997E+01 6.492E-01 +-8.413E-02 2.283E+01 3.230E-01 +-4.033E-02 2.604E+01 2.573E-01 +-3.335E-02 2.912E+01 2.277E-01 +-2.628E-02 3.200E+01 3.028E-01 +-3.073E-02 3.517E+01 1.907E-01 +-2.201E-02 4.051E+01 1.499E-01 +-1.943E-02 4.549E+01 8.145E-02 +-1.450E-02 \END; /* Data scanned from left hand side of Fig.2a, p231 in reference */ \\EXP,5; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,5; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'25',X%'26'); /* '25' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '26' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=2.821MEV; J-PTY=9/2+; TRNSF-L=4'27'; /* '27' Transferred orbital angular momentum (L) */ TRNSF-J=9/2'28'; /* '28' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.649E+00 4.069E-01 +-4.716E-02 7.569E+00 3.497E-01 +-3.610E-02 1.065E+01 3.303E-01 +-2.946E-02 1.392E+01 3.014E-01 +-2.409E-02 1.676E+01 3.436E-01 +-2.588E-02 1.990E+01 2.747E-01 +-1.199E-02 2.273E+01 2.114E-01 +-1.787E-02 2.602E+01 1.325E-01 +-1.367E-02 2.921E+01 1.059E-01 +-8.953E-03 3.215E+01 1.108E-01 +-6.328E-03 3.525E+01 8.169E-02 +-5.406E-03 4.062E+01 5.406E-02 +-5.074E-03 4.559E+01 3.399E-02 +-3.509E-03 \END; /* Data scanned from left hand side of Fig.2a, p231 in reference */ \\EXP,6; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,6; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'29',X%'30'); /* '29' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '30' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=3.330MEV; J-PTY=9/2+; TRNSF-L=4'31'; /* '31' Transferred orbital angular momentum (L) */ TRNSF-J=9/2'32'; /* '32' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.774E+00 2.693E-01 +-7.836E-03 1.393E+01 2.398E-01 +-2.155E-02 1.718E+01 1.785E-01 +-1.524E-02 2.318E+01 9.764E-02 +-7.904E-03 2.643E+01 7.508E-02 +-6.078E-03 2.913E+01 6.943E-02 +-6.549E-03 3.248E+01 6.743E-02 +-6.663E-03 3.553E+01 4.917E-02 +-5.080E-03 4.055E+01 5.332E-02 +-4.791E-03 4.547E+01 3.128E-02 +-2.951E-03 \END; /* Data scanned from left hand side of Fig.2a, p232 in reference */ \\EXP,7; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,7; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'33',X%'34'); /* '33' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '34' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=4.074MEV; J-PTY=9/2+; TRNSF-L=4'35'; /* '35' Transferred orbital angular momentum (L) */ TRNSF-J=9/2'36'; /* '36' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.855E+00 2.024E-01 +-4.110E-02 8.088E+00 2.163E-01 +-2.565E-02 1.089E+01 1.848E-01 +-1.961E-02 1.405E+01 1.776E-01 +-1.665E-02 1.733E+01 1.551E-01 +-1.266E-02 2.027E+01 1.318E-01 +-1.236E-02 2.935E+01 3.118E-02 +-3.502E-03 3.241E+01 4.770E-02 +-5.061E-03 3.558E+01 5.607E-02 +-4.727E-03 4.063E+01 3.806E-02 +-3.105E-03 4.547E+01 2.415E-02 +-2.563E-03 \END; /* Data scanned from left hand side of Fig.2a, p232 in reference */ \\EXP,8; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,8; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'37',X%'38'); /* '37' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '38' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=4.283MEV; J-PTY=9/2+; TRNSF-L=4'39'; /* '39' Transferred orbital angular momentum (L) */ TRNSF-J=9/2'40'; /* '40' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 5.04263E+00 2.05132E-01 +-4.53018E-02 8.18204E+00 1.76200E-01 +-1.75637E-02 1.10888E+01 1.68025E-01 +-2.20917E-02 1.42283E+01 1.54253E-01 +-2.02810E-02 1.74839E+01 1.25155E-01 +-1.51160E-02 2.02745E+01 1.19348E-01 +-1.06554E-02 2.36465E+01 7.35117E-02 +-6.56317E-03 2.64371E+01 6.31438E-02 +-6.29418E-03 3.28321E+01 3.47018E-02 +-3.09820E-03 3.57390E+01 3.50331E-02 +-3.12777E-03 4.07388E+01 2.95256E-02 +-3.56605E-03 4.59711E+01 2.13743E-02 +-2.35501E-03 \END; /* Data scanned from left hand side of Fig.2a, p232 in reference */ \\EXP,9; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,9; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'41',X%'42'); /* '41' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '42' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=7.026MEV; J-PTY=9/2+; TRNSF-L=4'43'; /* '43' Transferred orbital angular momentum (L) */ TRNSF-J=9/2'44'; /* '44' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.993E+00 4.124E-01 +-3.425E-02 8.015E+00 4.296E-01 +-4.065E-02 1.405E+01 3.891E-01 +-3.681E-02 1.726E+01 2.763E-01 +-2.294E-02 2.329E+01 2.145E-01 +-2.029E-02 \END; /* Data scanned from left hand side of Fig.2a, p232 in reference */ \\EXP,10; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,10; INC-ENGY-LAB=65MEV; SYS-ERR=X%'45'; /* '45' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=0.000MEV; J-PTY=9/2+; TRNSF-L=4'46'; /* '46' Transferred orbital angular momentum (L) */ TRNSF-J=9/2'47'; /* '47' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.726E+00 3.879E-02 +-2.069E-02 7.796E+00 5.439E-02 +-1.379E-02 1.081E+01 5.249E-02 +-2.724E-02 1.387E+01 1.649E-01 +-2.069E-02 1.687E+01 1.530E-01 +-2.143E-02 1.988E+01 1.238E-01 +-2.069E-02 2.304E+01 2.389E-02 +-1.907E-02 2.609E+01 -4.046E-02 +-2.452E-02 2.892E+01 -2.296E-02 +-2.180E-02 3.201E+01 8.157E-02 +-1.907E-02 3.537E+01 1.887E-01 +-1.907E-02 4.029E+01 1.260E-01 +-2.997E-02 4.531E+01 1.396E-01 +-1.907E-02 \END; /* Data scanned from right hand side of Fig.2a, p231 in reference */ \\EXP,11; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,11; INC-ENGY-LAB=65MEV; SYS-ERR=X%'48'; /* '48' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=1.902MEV; J-PTY=9/2+; TRNSF-L=4'49'; /* '49' Transferred orbital angular momentum (L) */ TRNSF-J=9/2'50'; /* '50' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.861E+00 -3.252E-03 +-9.061E-02 8.003E+00 2.159E-02 +-9.708E-02 1.084E+01 1.760E-01 +-9.385E-02 1.395E+01 2.017E-01 +-5.272E-02 1.712E+01 2.451E-01 +-5.825E-02 1.994E+01 8.233E-02 +-5.825E-02 2.314E+01 -3.200E-02 +-5.178E-02 2.622E+01 -6.650E-04 +-5.503E-02 2.898E+01 1.136E-02 +-5.501E-02 3.219E+01 4.265E-02 +-5.825E-02 3.533E+01 1.031E-01 +-7.119E-02 4.042E+01 5.932E-02 +-5.825E-02 4.519E+01 2.861E-02 +-8.090E-02 \END; /* Data scanned from right hand side of Fig.2a, p231 in reference */ \\EXP,12; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,12; INC-ENGY-LAB=65MEV; SYS-ERR=X%'51'; /* '51' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=2.226MEV; J-PTY=9/2+; TRNSF-L=4'52'; /* '52' Transferred orbital angular momentum (L) */ TRNSF-J=9/2'53'; /* '53' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.749E+00 -1.523E-01 +-2.117E-01 7.856E+00 2.088E-01 +-2.769E-01 1.088E+01 -1.272E-01 +-2.606E-01 1.392E+01 -6.260E-02 +-1.987E-01 1.708E+01 1.681E-01 +-1.726E-01 1.999E+01 1.481E-01 +-1.629E-01 2.308E+01 -8.764E-03 +-1.498E-01 2.618E+01 -9.072E-02 +-1.564E-01 2.896E+01 -1.433E-01 +-1.987E-01 3.212E+01 2.881E-02 +-1.824E-01 3.541E+01 -2.030E-01 +-1.759E-01 4.041E+01 1.545E-01 +-1.889E-01 4.533E+01 -2.112E-01 +-2.085E-01 \END; /* Data scanned from right hand side of Fig.2a, p231 in reference */ \\EXP,13; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,13; INC-ENGY-LAB=65MEV; SYS-ERR=X%'54'; /* '54' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=2.454MEV; J-PTY=9/2+; TRNSF-L=4'55'; /* '55' Transferred orbital angular momentum (L) */ TRNSF-J=9/2'56'; /* '56' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.755E+00 2.409E-02 +-2.265E-01 7.849E+00 -2.729E-02 +-2.337E-01 1.076E+01 -2.666E-01 +-2.072E-01 1.380E+01 1.736E-01 +-1.711E-01 1.704E+01 -1.067E-01 +-1.542E-01 1.981E+01 5.645E-02 +-1.349E-01 2.295E+01 5.325E-02 +-1.614E-01 2.604E+01 -2.704E-01 +-1.494E-01 2.881E+01 8.792E-02 +-1.687E-01 3.195E+01 1.980E-01 +-1.422E-01 3.513E+01 4.537E-02 +-1.639E-01 4.017E+01 -1.132E-02 +-1.855E-01 4.534E+01 3.798E-02 +-2.145E-01 \END; /* Data scanned from right hand side of Fig.2a, p231 in reference */ \\EXP,14; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,14; INC-ENGY-LAB=65MEV; SYS-ERR=X%'57'; /* '57' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=2.821MEV; J-PTY=9/2+; TRNSF-L=4'58'; /* '58' Transferred orbital angular momentum (L) */ TRNSF-J=9/2'59'; /* '59' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.859E+00 -8.065E-02 +-8.223E-02 7.809E+00 -5.536E-02 +-9.539E-02 1.075E+01 1.081E-01 +-9.868E-02 1.385E+01 7.965E-02 +-9.273E-02 1.702E+01 1.947E-01 +-7.565E-02 1.986E+01 5.890E-02 +-5.590E-02 2.300E+01 4.138E-02 +-6.250E-02 2.608E+01 4.133E-03 +-6.579E-02 2.884E+01 1.634E-02 +-7.237E-02 3.198E+01 6.131E-02 +-6.579E-02 3.512E+01 6.351E-02 +-6.908E-02 4.025E+01 2.591E-01 +-8.223E-02 4.535E+01 1.587E-01 +-1.020E-01 \END; /* Data scanned from right hand side of Fig.2a, p231 in reference */ \\EXP,15; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,15; INC-ENGY-LAB=65MEV; SYS-ERR=X%'60'; /* '60' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=3.330MEV; J-PTY=9/2+; TRNSF-L=4'61'; /* '61' Transferred orbital angular momentum (L) */ TRNSF-J=9/2'62'; /* '62' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.752E+00 2.595E-01 +-1.185E-01 1.387E+01 1.348E-01 +-8.276E-02 1.675E+01 2.326E-02 +-1.052E-01 2.310E+01 1.845E-01 +-7.158E-02 2.591E+01 -1.104E-01 +-8.699E-02 2.917E+01 1.066E-01 +-9.618E-02 3.227E+01 5.525E-02 +-9.609E-02 3.516E+01 2.166E-01 +-8.950E-02 4.042E+01 4.749E-02 +-9.394E-02 4.538E+01 2.623E-02 +-1.096E-01 \END; /* Data scanned from right hand side of Fig.2a, p232 in reference */ \\EXP,16; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,16; INC-ENGY-LAB=65MEV; SYS-ERR=X%'63'; /* '63' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=4.074MEV; J-PTY=9/2+; TRNSF-L=4'64'; /* '64' Transferred orbital angular momentum (L) */ TRNSF-J=9/2'65'; /* '65' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.739E+00 3.000E-01 +-1.435E-01 7.728E+00 -1.195E-02 +-1.247E-01 1.075E+01 6.425E-02 +-1.341E-01 1.395E+01 1.404E-01 +-1.012E-01 1.682E+01 1.578E-01 +-1.035E-01 2.001E+01 -8.412E-03 +-9.413E-02 2.913E+01 -1.610E-01 +-1.365E-01 3.229E+01 7.042E-02 +-1.082E-01 3.526E+01 5.253E-02 +-8.470E-02 4.045E+01 7.123E-02 +-1.059E-01 4.550E+01 8.764E-02 +-1.247E-01 \END; /* Data scanned from right hand side of Fig.2a, p232 in reference */ \\EXP,17; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,17; INC-ENGY-LAB=65MEV; SYS-ERR=X%'66'; /* '66' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=4.283MEV; J-PTY=9/2+; TRNSF-L=4'67'; /* '67' Transferred orbital angular momentum (L) */ TRNSF-J=9/2'68'; /* '68' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.860E+00 -5.694E-02 +-1.435E-01 7.710E+00 1.073E-02 +-1.435E-01 1.082E+01 4.645E-02 +-1.481E-01 1.404E+01 -6.592E-02 +-1.230E-01 1.685E+01 4.732E-02 +-1.230E-01 2.009E+01 -2.906E-01 +-8.656E-02 2.316E+01 9.596E-02 +-1.184E-01 2.595E+01 4.291E-02 +-9.567E-02 3.230E+01 5.965E-02 +-1.344E-01 3.528E+01 1.227E-01 +-1.253E-01 4.048E+01 2.217E-01 +-1.094E-01 4.546E+01 2.912E-01 +-1.184E-01 \END; /* Data scanned from right hand side of Fig.2a, p232 in reference */ \\EXP,18; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,18; INC-ENGY-LAB=65MEV; SYS-ERR=X%'69'; /* '69' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=7.026MEV; J-PTY=9/2+; TRNSF-L=4'70'; /* '70' Transferred orbital angular momentum (L) */ TRNSF-J=9/2'71'; /* '71' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.840E+00 6.423E-02 +-9.028E-02 1.399E+01 -6.651E-02 +-7.407E-02 1.708E+01 2.155E-01 +-7.176E-02 2.316E+01 -8.845E-02 +-6.944E-02 \END; /* Data scanned from right hand side of Fig.2a, p232 in reference */ \\EXP,19; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,19; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'72',X%'73'); /* '72' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '73' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=0.656MEV; J-PTY=1/2-; TRNSF-L=1'74'; /* '74' Transferred orbital angular momentum (L) */ TRNSF-J=1/2'75'; /* '75' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.677E+00 4.026E+00 +-1.350E-01 7.661E+00 3.825E+00 +-NEGLIGIBLE 1.065E+01 2.446E+00 +-8.200E-02 1.384E+01 1.473E+00 +-4.937E-02 1.683E+01 8.674E-01 +-2.908E-02 1.988E+01 6.614E-01 +-2.594E-02 2.313E+01 4.800E-01 +-1.882E-02 2.599E+01 3.408E-01 +-1.142E-02 2.917E+01 2.627E-01 +-8.807E-03 3.248E+01 1.927E-01 +-1.088E-02 3.534E+01 1.281E-01 +-5.758E-03 4.073E+01 8.504E-02 +-3.822E-03 4.573E+01 5.523E-02 +-4.745E-03 \END; /* Data scanned from left hand side of Fig.2b, p233 in reference */ \\EXP,20; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,20; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'76',X%'77'); /* '76' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '77' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=7.158MEV; J-PTY=1/2-; TRNSF-L=1'78'; /* '78' Transferred orbital angular momentum (L) */ TRNSF-J=1/2'79'; /* '79' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.907E+00 1.138E+00 +-5.870E-02 7.832E+00 7.342E-01 +-5.753E-02 1.414E+01 5.940E-01 +-2.840E-02 1.688E+01 2.420E-01 +-2.179E-02 2.316E+01 2.638E-01 +-1.261E-02 \END; /* Data scanned from left hand side of Fig.2b, p233 in reference */ \\EXP,21; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,21; INC-ENGY-LAB=65MEV; SYS-ERR=X%'80'; /* '80' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=0.656MEV; J-PTY=1/2-; TRNSF-L=1'81'; /* '81' Transferred orbital angular momentum (L) */ TRNSF-J=1/2'82'; /* '82' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.887E+00 -4.230E-01 +-2.902E-02 8.009E+00 -2.251E-01 +-3.348E-02 1.079E+01 1.136E-01 +-3.571E-02 1.409E+01 4.365E-01 +-4.241E-02 1.706E+01 2.327E-01 +-4.464E-02 1.999E+01 3.780E-02 +-4.911E-02 2.315E+01 -8.769E-04 +-4.241E-02 2.645E+01 4.537E-01 +-4.018E-02 2.927E+01 6.740E-01 +-4.687E-02 3.246E+01 4.858E-01 +-4.687E-02 3.521E+01 1.638E-01 +-6.250E-02 4.053E+01 1.692E-01 +-6.250E-02 4.557E+01 6.993E-01 +-6.473E-02 \END; /* Data scanned from right hand side of Fig.2b, p233 in reference */ \\EXP,22; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,22; INC-ENGY-LAB=65MEV; SYS-ERR=X%'83'; /* '83' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=7.158MEV; J-PTY=1/2-; TRNSF-L=1'84'; /* '84' Transferred orbital angular momentum (L) */ TRNSF-J=1/2'85'; /* '85' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.818E+00 -1.490E-01 +-5.200E-02 7.791E+00 -1.654E-02 +-6.382E-02 1.383E+01 2.366E-01 +-6.854E-02 1.699E+01 1.728E-01 +-9.454E-02 2.303E+01 2.886E-02 +-5.673E-02 \END; /* Data scanned from right hand side of Fig.2b, p233 in reference */ \\EXP,23; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,23; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'86',X%'87'); /* '86' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '87' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=1.158MEV; J-PTY=3/2-; TRNSF-L=1'88'; /* '88' Transferred orbital angular momentum (L) */ TRNSF-J=3/2'89'; /* '89' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.581E+00 4.890E+00 +-1.570E-01 7.526E+00 4.411E+00 +-2.037E-01 1.051E+01 2.849E+00 +-1.048E-01 1.381E+01 1.613E+00 +-5.932E-02 1.651E+01 1.210E+00 +-4.448E-02 1.975E+01 1.167E+00 +-2.664E-02 2.297E+01 9.191E-01 +-3.380E-02 2.590E+01 5.231E-01 +-2.415E-02 2.912E+01 3.302E-01 +-1.060E-02 3.220E+01 2.770E-01 +-1.019E-02 3.515E+01 2.602E-01 +-8.354E-03 4.055E+01 1.573E-01 +-6.521E-03 4.522E+01 7.765E-02 +-2.492E-03 \END; /* Data scanned from left hand side of Fig.2c, p234 in reference */ \\EXP,24; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,24; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'90',X%'91'); /* '90' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '91' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=2.084MEV; J-PTY=3/2-; TRNSF-L=1'92'; /* '92' Transferred orbital angular momentum (L) */ TRNSF-J=3/2'93'; /* '93' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.810E+00 4.320E-01 +-5.596E-02 7.647E+00 4.204E-01 +-3.188E-02 1.070E+01 2.378E-01 +-2.275E-02 1.385E+01 1.781E-01 +-1.585E-02 1.674E+01 1.601E-01 +-7.994E-03 2.003E+01 1.474E-01 +-1.022E-02 2.311E+01 1.124E-01 +-9.263E-03 2.591E+01 7.319E-02 +-5.071E-03 2.910E+01 4.016E-02 +-3.045E-03 3.227E+01 4.577E-02 +-2.579E-03 3.523E+01 4.320E-02 +-2.994E-03 4.037E+01 2.875E-02 +-1.992E-03 4.536E+01 1.537E-02 +-1.267E-03 \END; /* Data scanned from left hand side of Fig.2c, p234 in reference */ \\EXP,25; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,25; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'94',X%'95'); /* '94' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '95' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=2.901MEV; J-PTY=3/2-; TRNSF-L=1'96'; /* '96' Transferred orbital angular momentum (L) */ TRNSF-J=3/2'97'; /* '97' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.859E+00 4.139E-01 +-7.103E-02 7.733E+00 2.847E-01 +-2.916E-02 1.073E+01 1.786E-01 +-2.071E-02 1.394E+01 1.456E-01 +-1.104E-02 1.677E+01 1.217E-01 +-1.164E-02 1.982E+01 1.362E-01 +-9.440E-03 2.310E+01 1.111E-01 +-7.696E-03 2.591E+01 7.731E-02 +-5.862E-03 2.917E+01 4.940E-02 +-4.397E-03 3.224E+01 3.566E-02 +-3.412E-03 3.520E+01 5.753E-02 +-4.741E-03 4.039E+01 3.559E-02 +-3.405E-03 4.535E+01 2.742E-02 +-2.079E-03 \END; /* Data scanned from left hand side of Fig.2c, p234 in reference */ \\EXP,26; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,26; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'98',X%'99'); /* '98' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '99' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=3.187MEV; J-PTY=3/2-; TRNSF-L=1'100'; /* '100' Transferred orbital angular momentum (L) */ TRNSF-J=3/2'101'; /* '101' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 7.580E+00 2.007E-01 +-1.925E-02 1.066E+01 1.499E-01 +-1.239E-02 1.386E+01 8.102E-02 +-9.421E-03 1.671E+01 9.227E-02 +-9.470E-03 1.993E+01 7.507E-02 +-6.699E-03 2.308E+01 5.676E-02 +-4.315E-03 2.591E+01 4.592E-02 +-3.190E-03 2.914E+01 4.221E-02 +-3.209E-03 3.224E+01 3.541E-02 +-3.161E-03 3.519E+01 2.489E-02 +-2.555E-03 4.048E+01 2.240E-02 +-1.703E-03 4.544E+01 1.560E-02 +-1.601E-03 \END; /* Data scanned from left hand side of Fig.2c, p234 in reference */ \\EXP,27; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,27; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'102',X%'103'); /* '102' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '103' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=4.664MEV; J-PTY=3/2-; TRNSF-L=1'104'; /* '104' Transferred orbital angular momentum (L) */ TRNSF-J=3/2'105'; /* '105' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.669E+00 5.116E-01 +-4.071E-02 7.638E+00 4.679E-01 +-3.448E-02 1.089E+01 2.950E-01 +-2.174E-02 1.406E+01 2.203E-01 +-1.494E-02 1.698E+01 1.710E-01 +-1.160E-02 2.027E+01 1.530E-01 +-8.601E-03 2.330E+01 1.519E-01 +-8.538E-03 2.642E+01 9.841E-02 +-5.532E-03 2.933E+01 7.515E-02 +-4.660E-03 4.093E+01 2.654E-02 +-1.955E-03 4.568E+01 3.460E-02 +-2.347E-03 \END; /* Data scanned from left hand side of Fig.2c, p235 in reference */ \\EXP,28; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,28; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'106',X%'107'); /* '106' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '107' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=8.433MEV; J-PTY=3/2-; TRNSF-L=1'108'; /* '108' Transferred orbital angular momentum (L) */ TRNSF-J=3/2'109'; /* '109' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 1.079E+01 1.099E+00 +-6.165E-02 1.402E+01 3.764E-01 +-2.111E-02 1.680E+01 2.165E-01 +-1.089E-02 2.003E+01 2.183E-01 +-1.098E-02 2.319E+01 1.613E-01 +-8.117E-03 \END; /* Data scanned from left hand side of Fig.2c, p235 in reference */ \\EXP,29; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,29; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'110',X%'111'); /* '110' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '111' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=8.742MEV; J-PTY=3/2-; TRNSF-L=1'112'; /* '112' Transferred orbital angular momentum (L) */ TRNSF-J=3/2'113'; /* '113' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.498E+00 1.254E+00 +-4.689E-02 7.341E+00 1.353E+00 +-7.285E-02 1.656E+01 3.485E-01 +-1.685E-02 1.986E+01 4.286E-01 +-3.265E-02 2.289E+01 3.186E-01 +-1.019E-02 \END; /* Data scanned from left hand side of Fig.2c, p235 in reference */ \\EXP,30; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,30; INC-ENGY-LAB=65MEV; SYS-ERR=X%'114'; /* '114' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=1.158MEV; J-PTY=3/2-; TRNSF-L=1'115'; /* '115' Transferred orbital angular momentum (L) */ TRNSF-J=3/2'116'; /* '116' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.456E+00 2.192E-01 +-2.803E-02 7.617E+00 1.052E-01 +-2.570E-02 1.078E+01 -2.523E-02 +-2.103E-02 1.363E+01 -5.965E-02 +-2.803E-02 1.677E+01 2.095E-01 +-2.803E-02 1.992E+01 4.085E-01 +-2.103E-02 2.277E+01 4.208E-01 +-3.504E-02 2.589E+01 3.558E-01 +-2.570E-02 2.918E+01 2.113E-01 +-4.906E-02 3.204E+01 2.820E-01 +-4.672E-02 3.514E+01 4.390E-01 +-4.672E-02 4.013E+01 5.528E-01 +-5.607E-02 4.540E+01 2.576E-01 +-6.308E-02 \END; /* Data scanned from right hand side of Fig.2c, p234 in reference */ \\EXP,31; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,31; INC-ENGY-LAB=65MEV; SYS-ERR=X%'117'; /* '117' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=2.084MEV; J-PTY=3/2-; TRNSF-L=1'118'; /* '118' Transferred orbital angular momentum (L) */ TRNSF-J=3/2'119'; /* '119' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.420E+00 2.837E-01 +-9.648E-02 7.547E+00 2.539E-01 +-9.176E-02 1.074E+01 6.180E-02 +-1.223E-01 1.358E+01 -6.899E-02 +-1.200E-01 1.678E+01 1.177E-01 +-9.884E-02 1.986E+01 4.032E-01 +-8.470E-02 2.278E+01 4.959E-01 +-8.002E-02 2.590E+01 4.238E-01 +-1.012E-01 2.907E+01 3.987E-01 +-1.270E-01 3.191E+01 2.609E-01 +-1.130E-01 3.505E+01 3.111E-01 +-1.059E-01 4.007E+01 4.851E-01 +-1.247E-01 4.528E+01 4.614E-01 +-1.576E-01 \END; /* Data scanned from right hand side of Fig.2c, p234 in reference */ \\EXP,32; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,32; INC-ENGY-LAB=65MEV; SYS-ERR=X%'120'; /* '120' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=2.901MEV; J-PTY=3/2-; TRNSF-L=1'121'; /* '121' Transferred orbital angular momentum (L) */ TRNSF-J=3/2'122'; /* '122' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.583E+00 1.689E-01 +-1.130E-01 7.631E+00 -7.688E-02 +-1.200E-01 1.090E+01 2.255E-01 +-1.294E-01 1.372E+01 3.261E-03 +-1.271E-01 1.690E+01 -8.496E-02 +-1.247E-01 2.012E+01 4.564E-02 +-9.884E-02 2.298E+01 1.458E-01 +-8.707E-02 2.613E+01 1.682E-01 +-8.472E-02 2.936E+01 -1.201E-01 +-1.082E-01 3.227E+01 2.475E-02 +-1.200E-01 3.534E+01 2.919E-01 +-8.707E-02 4.051E+01 3.488E-01 +-1.106E-01 4.564E+01 2.152E-01 +-1.153E-01 \END; /* Data scanned from right hand side of Fig.2c, p234 in reference */ \\EXP,33; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,33; INC-ENGY-LAB=65MEV; SYS-ERR=X%'123'; /* '123' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=3.187MEV; J-PTY=3/2-; TRNSF-L=1'124'; /* '124' Transferred orbital angular momentum (L) */ TRNSF-J=3/2'125'; /* '125' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 7.564E+00 2.200E-01 +-1.303E-01 1.081E+01 2.235E-01 +-1.493E-01 1.367E+01 -2.065E-01 +-1.659E-01 1.682E+01 6.016E-02 +-1.327E-01 1.998E+01 3.813E-01 +-1.232E-01 2.290E+01 8.635E-02 +-1.232E-01 2.602E+01 1.539E-01 +-1.137E-01 2.927E+01 2.001E-01 +-1.209E-01 3.215E+01 2.109E-01 +-1.303E-01 3.522E+01 2.501E-01 +-1.446E-01 4.027E+01 4.259E-01 +-1.351E-01 4.554E+01 1.846E-01 +-1.564E-01 \END; /* Data scanned from right hand side of Fig.2c, p234 in reference */ \\EXP,34; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,34; INC-ENGY-LAB=65MEV; SYS-ERR=X%'126'; /* '126' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=4.664MEV; J-PTY=3/2-; TRNSF-L=1'127'; /* '127' Transferred orbital angular momentum (L) */ TRNSF-J=3/2'128'; /* '128' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.842E+00 2.295E-01 +-1.000E-01 7.738E+00 2.500E-02 +-8.636E-02 1.086E+01 -8.182E-02 +-1.091E-01 1.394E+01 -2.068E-01 +-1.000E-01 1.692E+01 3.636E-02 +-1.023E-01 2.000E+01 1.136E-02 +-9.318E-02 2.326E+01 2.023E-01 +-6.591E-02 2.620E+01 -3.182E-02 +-7.955E-02 2.928E+01 1.386E-01 +-8.864E-02 4.050E+01 1.705E-01 +-1.205E-01 4.543E+01 3.341E-01 +-9.773E-02 \END; /* Data scanned from right hand side of Fig.2c, p235 in reference */ \\EXP,35; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,35; INC-ENGY-LAB=65MEV; SYS-ERR=X%'129'; /* '129' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=8.433MEV; J-PTY=3/2-; TRNSF-L=1'130'; /* '130' Transferred orbital angular momentum (L) */ TRNSF-J=3/2'131'; /* '131' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 1.089E+01 -5.842E-02 +-5.787E-02 1.406E+01 -1.178E-01 +-7.870E-02 1.683E+01 3.924E-01 +-7.638E-02 2.005E+01 2.752E-01 +-6.018E-02 2.322E+01 1.857E-01 +-6.249E-02 \END; /* Data scanned from right hand side of Fig.2c, p235 in reference */ \\EXP,36; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,36; INC-ENGY-LAB=65MEV; SYS-ERR=X%'132'; /* '132' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=8.742MEV; J-PTY=3/2-; TRNSF-L=1'133'; /* '133' Transferred orbital angular momentum (L) */ TRNSF-J=3/2'134'; /* '134' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.919E+00 1.705E-01 +-4.369E-02 7.749E+00 1.330E-01 +-4.854E-02 1.706E+01 1.150E-01 +-5.825E-02 2.016E+01 3.274E-01 +-4.854E-02 2.318E+01 2.850E-01 +-5.097E-02 \END; /* Data scanned from right hand side of Fig.2c, p235 in reference */ \\EXP,37; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,37; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'135',X%'136'); /* '135' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '136' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=1.532MEV; J-PTY=5/2-; TRNSF-L=3'137'; /* '137' Transferred orbital angular momentum (L) */ TRNSF-J=5/2'138'; /* '138' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.726E+00 1.951E+00 +-1.767E-01 7.463E+00 1.329E+00 +-5.888E-02 1.056E+01 1.324E+00 +-5.864E-02 1.380E+01 1.209E+00 +-6.040E-02 1.690E+01 1.159E+00 +-4.480E-02 1.983E+01 8.850E-01 +-3.421E-02 2.296E+01 5.591E-01 +-1.847E-02 2.608E+01 3.551E-01 +-1.373E-02 2.906E+01 3.242E-01 +-1.253E-02 3.230E+01 2.700E-01 +-1.658E-02 3.504E+01 1.953E-01 +-1.312E-02 4.036E+01 1.202E-01 +-3.971E-03 4.534E+01 1.185E-01 +-5.920E-03 \END; /* Data scanned from left hand side of Fig.2d, p236 in reference */ \\EXP,38; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,38; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'139',X%'140'); /* '139' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '140' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=2.718MEV; J-PTY=5/2-; TRNSF-L=3'141'; /* '141' Transferred orbital angular momentum (L) */ TRNSF-J=5/2'142'; /* '142' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.658E+00 6.515E-01 +-9.757E-02 7.540E+00 4.749E-01 +-3.160E-02 1.068E+01 3.634E-01 +-2.836E-02 1.385E+01 3.878E-01 +-2.802E-02 1.686E+01 3.181E-01 +-2.116E-02 1.986E+01 2.460E-01 +-1.637E-02 2.314E+01 1.709E-01 +-8.457E-03 2.609E+01 1.200E-01 +-6.616E-03 2.928E+01 1.084E-01 +-8.462E-03 3.246E+01 1.028E-01 +-8.023E-03 3.523E+01 6.449E-02 +-5.032E-03 4.064E+01 4.963E-02 +-3.301E-03 4.564E+01 4.608E-02 +-3.065E-03 \END; /* Data scanned from left hand side of Fig.2d, p236 in reference */ \\EXP,39; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,39; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'143',X%'144'); /* '143' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '144' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=4.481MEV; J-PTY=5/2-; TRNSF-L=3'145'; /* '145' Transferred orbital angular momentum (L) */ TRNSF-J=5/2'146'; /* '146' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.559E+00 1.540E-01 +-2.495E-02 7.225E+00 1.714E-01 +-1.259E-02 1.045E+01 1.436E-01 +-1.983E-02 1.359E+01 1.112E-01 +-1.171E-02 1.651E+01 1.088E-01 +-1.196E-02 1.964E+01 1.046E-01 +-8.157E-03 2.583E+01 4.683E-02 +-4.501E-03 3.505E+01 3.833E-02 +-3.684E-03 4.040E+01 1.962E-02 +-1.886E-03 4.535E+01 1.764E-02 +-1.375E-03 \END; /* Data scanned from left hand side of Fig.2d, p236 in reference */ \\EXP,40; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,40; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'147',X%'148'); /* '147' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '148' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=8.938MEV; J-PTY=5/2-; TRNSF-L=3'149'; /* '149' Transferred orbital angular momentum (L) */ TRNSF-J=5/2'150'; /* '150' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.739E+00 8.789E-01 +-7.507E-02 7.463E+00 7.382E-01 +-3.375E-02 1.366E+01 7.258E-01 +-5.034E-02 1.677E+01 4.062E-01 +-2.495E-02 1.983E+01 4.754E-01 +-1.989E-02 2.310E+01 2.027E-01 +-1.245E-02 \END; /* Data scanned from left hand side of Fig.2d, p236 in reference */ \\EXP,41; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,41; INC-ENGY-LAB=65MEV; SYS-ERR=X%'151'; /* '151' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=1.532MEV; J-PTY=5/2-; TRNSF-L=3'152'; /* '152' Transferred orbital angular momentum (L) */ TRNSF-J=5/2'153'; /* '153' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.769E+00 8.367E-02 +-4.587E-02 7.628E+00 -1.199E-02 +-5.504E-02 1.084E+01 -2.073E-03 +-5.275E-02 1.393E+01 -1.390E-01 +-4.128E-02 1.683E+01 -2.163E-01 +-4.359E-02 1.996E+01 -3.394E-01 +-4.128E-02 2.317E+01 -2.125E-01 +-4.358E-02 2.592E+01 -1.004E-02 +-5.046E-02 2.910E+01 -1.240E-01 +-5.046E-02 3.236E+01 -3.836E-02 +-4.816E-02 3.521E+01 -7.210E-02 +-4.816E-02 4.059E+01 2.204E-01 +-5.275E-02 4.558E+01 7.022E-02 +-5.046E-02 \END; /* Data scanned from right hand side of Fig.2d, p236 in reference */ \\EXP,42; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,42; INC-ENGY-LAB=65MEV; SYS-ERR=X%'154'; /* '154' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=2.718MEV; J-PTY=5/2-; TRNSF-L=3'155'; /* '155' Transferred orbital angular momentum (L) */ TRNSF-J=5/2'156'; /* '156' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.770E+00 4.504E-02 +-7.972E-02 7.581E+00 1.124E-01 +-8.883E-02 1.076E+01 -4.130E-02 +-9.567E-02 1.389E+01 1.913E-02 +-8.656E-02 1.688E+01 -1.413E-01 +-6.833E-02 1.988E+01 -2.289E-01 +-6.150E-02 2.314E+01 -1.731E-01 +-6.833E-02 2.595E+01 -1.240E-01 +-6.378E-02 2.904E+01 -1.091E-01 +-6.606E-02 3.235E+01 -1.922E-01 +-6.150E-02 3.516E+01 -6.334E-02 +-8.200E-02 4.051E+01 3.733E-02 +-8.883E-02 4.527E+01 1.997E-01 +-8.200E-02 \END; /* Data scanned from right hand side of Fig.2d, p236 in reference */ \\EXP,43; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,43; INC-ENGY-LAB=65MEV; SYS-ERR=X%'157'; /* '157' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=4.481MEV; J-PTY=5/2-; TRNSF-L=3'158'; /* '158' Transferred orbital angular momentum (L) */ TRNSF-J=5/2'159'; /* '159' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.890E+00 -1.250E-02 +-1.225E-01 7.678E+00 1.150E-01 +-1.350E-01 1.090E+01 -2.000E-02 +-1.500E-01 1.409E+01 2.250E-02 +-1.425E-01 1.696E+01 -1.500E-01 +-1.225E-01 2.004E+01 -3.225E-01 +-1.075E-01 2.610E+01 -3.075E-01 +-1.025E-01 3.531E+01 -3.500E-02 +-1.150E-01 4.063E+01 1.675E-01 +-1.475E-01 4.556E+01 2.825E-01 +-1.375E-01 \END; /* Data scanned from right hand side of Fig.2d, p236 in reference */ \\EXP,44; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,44; INC-ENGY-LAB=65MEV; SYS-ERR=X%'160'; /* '160' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=8.938MEV; J-PTY=5/2-; TRNSF-L=3'161'; /* '161' Transferred orbital angular momentum (L) */ TRNSF-J=5/2'162'; /* '162' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.826E+00 2.685E-02 +-6.542E-02 7.608E+00 1.116E-01 +-6.776E-02 1.386E+01 1.061E-01 +-5.841E-02 1.678E+01 -5.207E-02 +-6.308E-02 1.988E+01 -4.198E-02 +-4.906E-02 2.317E+01 -2.935E-01 +-5.607E-02 \END; /* Data scanned from right hand side of Fig.2d, p236 in reference */ \\EXP,45; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,45; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'163',X%'164'); /* '163' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '164' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=3.456MEV; J-PTY=7/2-; TRNSF-L=3'165'; /* '165' Transferred orbital angular momentum (L) */ TRNSF-J=7/2'166'; /* '166' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 7.480E+00 4.465E-01 +-2.896E-02 1.063E+01 4.760E-01 +-3.653E-02 1.681E+01 2.536E-01 +-1.545E-02 2.001E+01 1.910E-01 +-1.239E-02 2.322E+01 1.336E-01 +-6.578E-03 2.634E+01 9.077E-02 +-6.244E-03 2.916E+01 1.130E-01 +-6.442E-03 3.246E+01 8.054E-02 +-6.823E-03 3.536E+01 7.217E-02 +-4.397E-03 4.064E+01 5.502E-02 +-3.351E-03 4.563E+01 4.582E-02 +-3.698E-03 \END; /* Data scanned from left hand side of Fig.2e, p237 in reference */ \\EXP,46; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,46; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'167',X%'168'); /* '167' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '168' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=3.591MEV; J-PTY=7/2-; TRNSF-L=3'169'; /* '169' Transferred orbital angular momentum (L) */ TRNSF-J=7/2'170'; /* '170' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.816E+00 8.700E-02 +-2.133E-02 7.666E+00 9.061E-02 +-1.529E-02 1.081E+01 8.837E-02 +-1.516E-02 1.389E+01 1.196E-01 +-1.224E-02 2.011E+01 7.020E-02 +-5.939E-03 2.304E+01 6.563E-02 +-4.691E-03 2.629E+01 5.017E-02 +-4.824E-03 2.922E+01 4.877E-02 +-4.341E-03 3.241E+01 2.941E-02 +-3.276E-03 3.520E+01 2.683E-02 +-3.107E-03 4.055E+01 1.913E-02 +-2.045E-03 4.562E+01 1.645E-02 +-1.981E-03 \END; /* Data scanned from left hand side of Fig.2e, p237 in reference */ \\EXP,47; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,47; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'171',X%'172'); /* '171' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '172' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=3.823MEV; J-PTY=7/2-; TRNSF-L=3'173'; /* '173' Transferred orbital angular momentum (L) */ TRNSF-J=7/2'174'; /* '174' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.501E+00 1.960E-01 +-3.531E-02 7.241E+00 2.705E-01 +-2.064E-02 1.059E+01 8.811E-02 +-1.307E-02 1.382E+01 1.369E-01 +-1.025E-02 1.655E+01 8.408E-02 +-7.458E-03 2.313E+01 3.905E-02 +-3.463E-03 2.625E+01 5.048E-02 +-3.501E-03 2.921E+01 4.425E-02 +-3.720E-03 3.235E+01 3.170E-02 +-3.214E-03 3.523E+01 2.404E-02 +-2.808E-03 4.065E+01 1.657E-02 +-1.779E-03 4.562E+01 1.388E-02 +-1.955E-03 \END; /* Data scanned from left hand side of Fig.2e, p237 in reference */ \\EXP,48; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,48; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'175',X%'176'); /* '175' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '176' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=4.796MEV; J-PTY=7/2-; TRNSF-L=3'177'; /* '177' Transferred orbital angular momentum (L) */ TRNSF-J=7/2'178'; /* '178' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.537E+00 3.091E-02 +-5.269E-03 7.324E+00 3.019E-02 +-2.607E-03 1.063E+01 2.468E-02 +-2.579E-03 1.371E+01 2.545E-02 +-1.969E-03 1.665E+01 1.807E-02 +-1.078E-03 1.984E+01 1.206E-02 +-8.794E-04 2.301E+01 9.695E-03 +-7.071E-04 2.628E+01 5.437E-03 +-3.486E-04 2.911E+01 5.444E-03 +-3.490E-04 3.229E+01 5.231E-03 +-3.354E-04 4.045E+01 1.888E-03 +-1.886E-04 4.535E+01 2.151E-03 +-1.858E-04 \END; /* Data scanned from left hand side of Fig.2e, p237 in reference */ \\EXP,49; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,49; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'179',X%'180'); /* '179' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '180' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=5.295MEV; J-PTY=7/2-; TRNSF-L=3'181'; /* '181' Transferred orbital angular momentum (L) */ TRNSF-J=7/2'182'; /* '182' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.706E+00 1.553E-02 +-1.785E-03 7.566E+00 1.064E-02 +-1.616E-03 1.065E+01 1.613E-02 +-1.919E-03 1.387E+01 1.388E-02 +-1.428E-03 1.667E+01 1.157E-02 +-1.190E-03 1.997E+01 7.613E-03 +-5.430E-04 2.323E+01 2.973E-03 +-4.145E-04 2.632E+01 4.145E-03 +-3.279E-04 2.931E+01 4.632E-03 +-3.484E-04 3.244E+01 4.350E-03 +-3.612E-04 3.542E+01 3.334E-03 +-2.378E-04 4.562E+01 2.134E-03 +-1.522E-04 \END; /* Data scanned from left hand side of Fig.2e, p237 in reference */ \\EXP,50; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,50; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'183',X%'184'); /* '183' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '184' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=5.394MEV; J-PTY=7/2-; TRNSF-L=3'185'; /* '185' Transferred orbital angular momentum (L) */ TRNSF-J=7/2'186'; /* '186' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.728E+00 3.447E-01 +-2.905E-02 7.578E+00 2.975E-01 +-1.989E-02 1.386E+01 2.996E-01 +-2.349E-02 1.660E+01 1.529E-01 +-1.087E-02 2.003E+01 1.675E-01 +-1.256E-02 2.319E+01 1.172E-01 +-5.830E-03 2.610E+01 5.531E-02 +-4.016E-03 2.927E+01 4.956E-02 +-3.315E-03 3.258E+01 3.162E-02 +-3.035E-03 3.543E+01 2.927E-02 +-2.645E-03 \END; /* Data scanned from left hand side of Fig.2e, p238 in reference */ \\EXP,51; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,51; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'187',X%'188'); /* '187' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '188' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=5.516MEV; J-PTY=7/2-; TRNSF-L=3'189'; /* '189' Transferred orbital angular momentum (L) */ TRNSF-J=7/2'190'; /* '190' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.787E+00 3.533E-01 +-2.770E-02 7.503E+00 3.523E-01 +-2.558E-02 1.378E+01 3.776E-01 +-2.961E-02 1.656E+01 1.651E-01 +-1.390E-02 1.992E+01 2.131E-01 +-1.671E-02 2.303E+01 1.226E-01 +-9.612E-03 2.600E+01 4.158E-02 +-4.485E-03 2.911E+01 3.623E-02 +-3.264E-03 3.234E+01 2.084E-02 +-3.265E-03 3.512E+01 2.100E-02 +-2.645E-03 \END; /* Data scanned from left hand side of Fig.2e, p238 in reference */ \\EXP,52; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,52; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'191',X%'192'); /* '191' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '192' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=5.690MEV; J-PTY=7/2-; TRNSF-L=3'193'; /* '193' Transferred orbital angular momentum (L) */ TRNSF-J=7/2'194'; /* '194' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.752E+00 2.516E-01 +-1.774E-02 7.616E+00 2.290E-01 +-1.895E-02 1.394E+01 2.335E-01 +-1.648E-02 1.671E+01 1.547E-01 +-1.217E-02 1.985E+01 1.478E-01 +-8.640E-03 2.320E+01 9.898E-02 +-6.581E-03 \END; /* Data scanned from left hand side of Fig.2e, p238 in reference */ \\EXP,53; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,53; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'195',X%'196'); /* '195' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '196' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=5.930MEV; J-PTY=7/2-; TRNSF-L=3'197'; /* '197' Transferred orbital angular momentum (L) */ TRNSF-J=7/2'198'; /* '198' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.793E+00 4.577E-01 +-3.801E-02 7.644E+00 3.722E-01 +-2.333E-02 1.390E+01 3.838E-01 +-1.790E-02 1.666E+01 2.485E-01 +-1.358E-02 1.987E+01 1.789E-01 +-1.121E-02 2.317E+01 1.348E-01 +-7.365E-03 \END; /* Data scanned from left hand side of Fig.2e, p238 in reference */ \\EXP,54; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,54; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'199',X%'200'); /* '199' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '200' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=6.070MEV; J-PTY=7/2-; TRNSF-L=3'201'; /* '201' Transferred orbital angular momentum (L) */ TRNSF-J=7/2'202'; /* '202' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.940E+00 3.803E-01 +-3.610E-02 7.743E+00 2.543E-01 +-2.414E-02 1.396E+01 3.361E-01 +-2.336E-02 1.679E+01 1.666E-01 +-1.295E-02 2.003E+01 1.485E-01 +-1.218E-02 2.314E+01 8.702E-02 +-8.422E-03 \END; /* Data scanned from left hand side of Fig.2e, p238 in reference */ \\EXP,55; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,55; INC-ENGY-LAB=65MEV; SYS-ERR=X%'203'; /* '203' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=3.456MEV; J-PTY=7/2-; TRNSF-L=3'204'; /* '204' Transferred orbital angular momentum (L) */ TRNSF-J=7/2'205'; /* '205' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 7.876E+00 -1.155E-01 +-8.746E-02 1.095E+01 -9.044E-03 +-8.010E-02 1.701E+01 -7.623E-02 +-9.302E-02 2.014E+01 -1.718E-01 +-7.494E-02 2.329E+01 -7.364E-02 +-9.044E-02 2.610E+01 9.044E-03 +-7.494E-02 2.926E+01 5.814E-02 +-8.010E-02 3.242E+01 9.948E-02 +-9.302E-02 3.531E+01 -6.460E-03 +-9.044E-02 4.051E+01 2.442E-01 +-9.302E-02 4.547E+01 2.132E-01 +-9.302E-02 \END; /* Data scanned from right hand side of Fig.2e, p237 in reference */ \\EXP,56; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,56; INC-ENGY-LAB=65MEV; SYS-ERR=X%'206'; /* '206' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=3.591MEV; J-PTY=7/2-; TRNSF-L=3'207'; /* '207' Transferred orbital angular momentum (L) */ TRNSF-J=7/2'208'; /* '208' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.796E+00 1.031E-01 +-1.655E-01 7.661E+00 7.221E-03 +-1.958E-01 1.078E+01 -1.180E-02 +-1.981E-01 1.406E+01 6.939E-02 +-1.352E-01 2.004E+01 -3.156E-02 +-1.212E-01 2.325E+01 -2.496E-02 +-1.119E-01 2.594E+01 2.684E-01 +-1.049E-01 2.924E+01 3.026E-02 +-1.212E-01 3.235E+01 6.952E-02 +-1.352E-01 3.522E+01 1.671E-01 +-1.282E-01 4.036E+01 2.177E-01 +-1.538E-01 4.545E+01 2.521E-01 +-1.515E-01 \END; /* Data scanned from right hand side of Fig.2e, p237 in reference */ \\EXP,57; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,57; INC-ENGY-LAB=65MEV; SYS-ERR=X%'209'; /* '209' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=3.823MEV; J-PTY=7/2-; TRNSF-L=3'210'; /* '210' Transferred orbital angular momentum (L) */ TRNSF-J=7/2'211'; /* '211' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.682E+00 1.059E-01 +-1.227E-01 7.648E+00 -1.018E-02 +-1.134E-01 1.075E+01 1.168E-01 +-1.968E-01 1.389E+01 3.075E-02 +-1.157E-01 1.683E+01 4.197E-02 +-1.389E-01 2.314E+01 -1.201E-02 +-1.481E-01 2.593E+01 5.710E-02 +-1.042E-01 2.913E+01 1.493E-01 +-1.180E-01 3.225E+01 1.651E-01 +-1.343E-01 3.517E+01 4.443E-02 +-1.528E-01 4.045E+01 3.725E-01 +-1.458E-01 4.548E+01 1.265E-01 +-1.644E-01 \END; /* Data scanned from right hand side of Fig.2e, p237 in reference */ \\EXP,58; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,58; INC-ENGY-LAB=65MEV; SYS-ERR=X%'212'; /* '212' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=4.796MEV; J-PTY=7/2-; TRNSF-L=3'213'; /* '213' Transferred orbital angular momentum (L) */ TRNSF-J=7/2'214'; /* '214' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.736E+00 1.183E-01 +-1.124E-01 7.558E+00 -1.756E-02 +-1.171E-01 1.074E+01 -3.162E-02 +-1.241E-01 1.394E+01 3.548E-01 +-1.007E-01 1.682E+01 7.845E-02 +-9.836E-02 2.000E+01 -2.927E-02 +-8.899E-02 2.309E+01 1.991E-02 +-9.133E-02 2.600E+01 -9.016E-02 +-1.054E-01 2.921E+01 2.564E-01 +-9.602E-02 3.229E+01 3.501E-01 +-1.148E-01 4.047E+01 3.126E-01 +-1.522E-01 4.560E+01 2.190E-01 +-1.358E-01 \END; /* Data scanned from right hand side of Fig.2e, p237 in reference */ \\EXP,59; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,59; INC-ENGY-LAB=65MEV; SYS-ERR=X%'215'; /* '215' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=5.295MEV; J-PTY=7/2-; TRNSF-L=3'216'; /* '216' Transferred orbital angular momentum (L) */ TRNSF-J=7/2'217'; /* '217' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.752E+00 1.690E-01 +-1.432E-01 7.733E+00 -2.066E-01 +-1.761E-01 1.076E+01 7.042E-03 +-1.385E-01 1.394E+01 3.991E-02 +-1.244E-01 1.673E+01 7.746E-02 +-1.174E-01 2.001E+01 -2.254E-01 +-1.150E-01 2.316E+01 -2.207E-01 +-1.620E-01 2.594E+01 -1.972E-01 +-1.197E-01 2.905E+01 2.113E-02 +-1.174E-01 3.222E+01 1.854E-01 +-1.197E-01 3.516E+01 -2.230E-01 +-1.150E-01 4.543E+01 -3.521E-01 +-1.268E-01 \END; /* Data scanned from right hand side of Fig.2e, p237 in reference */ \\EXP,60; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,60; INC-ENGY-LAB=65MEV; SYS-ERR=X%'218'; /* '218' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=5.394MEV; J-PTY=7/2-; TRNSF-L=3'219'; /* '219' Transferred orbital angular momentum (L) */ TRNSF-J=7/2'220'; /* '220' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.612E+00 -4.105E-02 +-1.103E-01 7.714E+00 1.218E-02 +-1.127E-01 1.379E+01 7.642E-02 +-7.512E-02 1.699E+01 -6.051E-02 +-1.127E-01 1.995E+01 2.326E-02 +-8.451E-02 2.301E+01 3.660E-02 +-9.155E-02 2.621E+01 -6.277E-02 +-1.080E-01 2.900E+01 -7.119E-03 +-1.103E-01 3.214E+01 1.658E-01 +-1.338E-01 3.535E+01 -1.002E-01 +-1.291E-01 \END; /* Data scanned from right hand side of Fig.2e, p238 in reference */ \\EXP,61; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,61; INC-ENGY-LAB=65MEV; SYS-ERR=X%'221'; /* '221' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=5.516MEV; J-PTY=7/2-; TRNSF-L=3'222'; /* '222' Transferred orbital angular momentum (L) */ TRNSF-J=7/2'223'; /* '223' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.727E+00 -2.293E-03 +-9.767E-02 7.818E+00 -1.307E-02 +-9.999E-02 1.391E+01 6.310E-02 +-7.906E-02 1.705E+01 1.174E-01 +-1.070E-01 1.991E+01 -4.905E-02 +-6.511E-02 2.314E+01 1.773E-01 +-7.674E-02 2.627E+01 2.130E-01 +-1.232E-01 2.909E+01 -5.574E-02 +-1.325E-01 3.218E+01 1.869E-01 +-1.628E-01 3.545E+01 3.424E-02 +-1.535E-01 \END; /* Data scanned from right hand side of Fig.2e, p238 in reference */ \\EXP,62; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,62; INC-ENGY-LAB=65MEV; SYS-ERR=X%'224'; /* '224' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=5.690MEV; J-PTY=7/2-; TRNSF-L=3'225'; /* '225' Transferred orbital angular momentum (L) */ TRNSF-J=7/2'226'; /* '226' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.794E+00 6.091E-02 +-1.276E-01 7.940E+00 -1.645E-01 +-1.206E-01 1.394E+01 -1.443E-02 +-9.745E-02 1.714E+01 8.496E-02 +-1.044E-01 2.003E+01 2.331E-01 +-8.817E-02 2.313E+01 2.304E-01 +-8.817E-02 \END; /* Data scanned from right hand side of Fig.2e, p238 in reference */ \\EXP,63; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,63; INC-ENGY-LAB=65MEV; SYS-ERR=X%'227'; /* '227' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=5.930MEV; J-PTY=7/2-; TRNSF-L=3'228'; /* '228' Transferred orbital angular momentum (L) */ TRNSF-J=7/2'229'; /* '229' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.646E+00 1.975E-01 +-7.942E-02 7.791E+00 1.375E-03 +-9.344E-02 1.384E+01 -5.434E-02 +-8.410E-02 1.697E+01 1.186E-01 +-8.646E-02 1.990E+01 1.072E-01 +-7.709E-02 2.307E+01 1.727E-01 +-7.942E-02 \END; /* Data scanned from right hand side of Fig.2e, p238 in reference */ \\EXP,64; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,64; INC-ENGY-LAB=65MEV; SYS-ERR=X%'230'; /* '230' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=6.070MEV; J-PTY=7/2-; TRNSF-L=3'231'; /* '231' Transferred orbital angular momentum (L) */ TRNSF-J=7/2'232'; /* '232' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.752E+00 9.757E-02 +-1.025E-01 7.856E+00 3.500E-03 +-1.150E-01 1.394E+01 7.292E-02 +-7.749E-02 1.714E+01 3.800E-03 +-8.999E-02 2.006E+01 -3.517E-02 +-8.999E-02 2.317E+01 8.249E-03 +-9.499E-02 \END; /* Data scanned from right hand side of Fig.2e, p238 in reference */ \\EXP,65; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,65; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'233',X%'234'); /* '233' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '234' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=1.365MEV; J-PTY=5/2+; TRNSF-L=2'235'; /* '235' Transferred orbital angular momentum (L) */ TRNSF-J=5/2'236'; /* '236' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.760E+00 3.791E-01 +-5.016E-02 7.601E+00 4.179E-01 +-3.538E-02 1.081E+01 3.732E-01 +-2.966E-02 1.407E+01 2.107E-01 +-1.782E-02 1.686E+01 1.167E-01 +-9.873E-03 2.001E+01 1.023E-01 +-8.650E-03 2.328E+01 1.252E-01 +-9.296E-03 2.611E+01 9.192E-02 +-7.306E-03 2.939E+01 6.104E-02 +-4.534E-03 3.242E+01 3.513E-02 +-3.521E-03 3.527E+01 4.081E-02 +-4.091E-03 4.052E+01 2.770E-02 +-2.631E-03 4.559E+01 1.818E-02 +-2.307E-03 \END; /* Data scanned from left hand side of Fig.2f, p239 in reference */ \\EXP,66; RCT=92MO(P,D)91MO; PHQ=ANGL-DSTRN; MONTR-RCT=/ 92MO(P,P)92MO /; \\DATA,66; INC-ENGY-LAB=65MEV; SYS-ERR=(<25%'237',X%'238'); /* '237' Total systematic error. Mainly due to the ambiguity of the procedure for fitting the theoretical to the experimental angular distributions */ /* '238' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=3.649MEV; J-PTY=5/2+; TRNSF-L=2'239'; /* '239' Transferred orbital angular momentum (L) */ TRNSF-J=5/2'240'; /* '240' Transferred total angular momentum (J) */ \DATA; THTC DSIGMA/DOMEGA DELTA-DSIGMA/DOMEGA (DEG) (MB/SR) (MB/SR) 4.622E+00 8.445E-01 +-2.599E-01 7.346E+00 8.143E-01 +-1.415E-01 1.060E+01 1.069E+00 +-1.626E-01 1.357E+01 8.181E-01 +-1.105E-01 1.986E+01 5.987E-01 +-6.335E-02 2.317E+01 3.476E-01 +-3.821E-02 2.600E+01 3.875E-01 +-3.941E-02 2.928E+01 2.554E-01 +-2.914E-02 3.239E+01 2.043E-01 +-2.674E-02 3.520E+01 1.926E-01 +-2.765E-02 4.055E+01 1.044E-01 +-1.723E-02 4.551E+01 1.094E-01 +-1.663E-02 \END; /* Data scanned from left hand side of Fig.2f, p239 in reference */ \\EXP,67; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,67; INC-ENGY-LAB=65MEV; SYS-ERR=X%'241'; /* '241' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=1.365MEV; J-PTY=5/2+; TRNSF-L=2'242'; /* '242' Transferred orbital angular momentum (L) */ TRNSF-J=5/2'243'; /* '243' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.412E+00 2.155E-01 +-9.514E-02 7.668E+00 1.362E-01 +-8.354E-02 1.055E+01 -4.479E-02 +-9.514E-02 1.376E+01 -7.298E-02 +-1.067E-01 1.701E+01 -2.149E-01 +-1.137E-01 1.959E+01 3.746E-01 +-9.742E-02 2.281E+01 3.556E-01 +-7.191E-02 2.602E+01 2.880E-01 +-7.887E-02 2.864E+01 2.325E-01 +-9.510E-02 3.194E+01 1.161E-01 +-1.276E-01 3.506E+01 3.663E-01 +-1.090E-01 4.006E+01 4.109E-01 +-1.044E-01 4.504E+01 3.557E-01 +-1.438E-01 \END; /* Data scanned from right hand side of Fig.2f, p239 in reference */ \\EXP,68; RCT=92MO(P,D)91MO; PHQ=VCTR-ANALPW; \\DATA,68; INC-ENGY-LAB=65MEV; SYS-ERR=X%'244'; /* '244' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; EXC-ENGY=3.649MEV; J-PTY=5/2+; TRNSF-L=2'245'; /* '245' Transferred orbital angular momentum (L) */ TRNSF-J=5/2'246'; /* '246' Transferred total angular momentum (J) */ \DATA; THTC AY DELTA-AY (DEG) (NODIM) (NODIM) 4.484E+00 -1.084E-01 +-1.884E-01 7.699E+00 4.237E-02 +-2.139E-01 1.057E+01 3.999E-02 +-1.697E-01 1.378E+01 -1.068E-01 +-1.674E-01 1.976E+01 2.277E-01 +-1.302E-01 2.294E+01 1.530E-01 +-1.465E-01 2.613E+01 1.340E-01 +-1.255E-01 2.932E+01 -1.221E-01 +-1.604E-01 3.206E+01 1.593E-01 +-1.604E-01 3.523E+01 3.032E-01 +-1.651E-01 4.023E+01 5.199E-01 +-1.883E-01 4.550E+01 1.528E-01 +-1.860E-01 \END; /* Data scanned from right hand side of Fig.2f, p239 in reference */ \\EXP,69; RCT=92MO(P,D)91MO; PHQ=SPEC-FCTR; \\DATA,69; INC-ENGY-LAB=65MEV; SYS-ERR=X%'247'; /* '247' Uncertainty in run-to-run variations of the integrated beam current are on the order of a few percent. */ EMT=D; \DATA; EXC-ENGY TRNSF-L TRNSF-J'248' SPEC-FCTR (MEV) (NODIM) (NODIM) (NODIM) 0.000 4 9/2 6.092 0.656 1 1/2 1.575 1.158 1 3/2 1.759 1.365 2 5/2 0.118 1.532 3 5/2 2.319 1.902 4 9/2 0.508 2.084 1 3/2 0.159 2.226 4 9/2 0.068 2.304 4 9/2 0.401 2.304 1 1/2 0.0456 2.454 4 9/2 0.101 2.718 3 5/2 0.733 2.821 4 9/2 0.406 2.901 1 3/2 0.147 3.187 1 3/2 0.0791 3.330 4 9/2 0.271 3.456 3 7/2 0.922 3.591 3 7/2 0.197 3.649 2 5/2 0.0314 3.823 3 7/2 0.339 3.956 4 9/2 0.170 3.956 3 7/2 0.0729 4.074 4 9/2 0.244 4.151 3 7/2 0.139 4.151 4 9/2 0.135 4.283 4 9/2 0.203 4.383 3 7/2 0.148 4.383 3 5/2 0.109 4.481 3 5/2 0.235 4.664 1 3/2 0.176 4.796 3 7/2 0.490 5.295 3 7/2 0.255 5.394 3 7/2 0.535 5.516 3 7/2 0.657 5.690 3 7/2 0.431 5.930 3 7/2 0.691 6.070 3 7/2 0.581 7.026 4 9/2 0.229 7.158 1 1/2 0.246 8.433 1 3/2 0.183 8.742 1 3/2 0.257 8.938 3 5/2 0.679 \END; /* Data taken from Table 1, p240 - p242 in reference */ /* '248' Transferred angular momentum j */ \\END;