000			00568pam a2200145a 44500
082			_aNASA _bMEMO 12-11-58E
100			_aHendricks,Robert C,Ehlers,Robert C
245	1		_aEVALUATION OF INJECTOR PRINCIPLES IN A 2400-POUND-THRUST ROCKET ENGINE USINJG LIQUID OXYGEN AND LIQUID AMMONIA
260			_a _bNasa, Washington, D.C. _c1959
300			_a33
500			_aBound With Nasa Memo 12-8-58e-12-10-58e, 12-13-58e-12-29-58e Lack No.12-9-58e, 12-12-58e, 12-14-58e-12-20-58e, 12-25-58e-12-28-58e.
700			_aGraham,Robert W
964			_gCIRC
997			_aTR14064 C
999			_c398726 _d398726