/* 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;