000 00467pam a2200133a 44500
008 160510b xxu||||| |||| 00| 0 eng d
082 _aNASA CR-1011
100 _aBENDER,D F,BLACKFORD,A L
245 _aGUIANCE,FLIGHT MECHANICS AND TRAJECTORY OPTIMIZATION.VOL-XII-RELATIVE MOTION,GUIDENCE EQUATIONS FOR TERMINAL RENDEZVOUS.
_b
260 _a
_bNASA,WASHINGTON, D.C.
_c1968
300 _a,90,,,,,,
500 _aBound with NASA CR-1012-1020.
650 _aCHEMISTRY, ORGANIC
999 _c479829
_d479829