000			00477pam a2200145a 44500
082			_aNASA _bTN D-4733
100			_aWanhainen,John P,Feiler,Charles E
245	1		_aEFFECT OF CHAMBER PRESSURE, FLOW PER ELEMENT, AND CONTRACTION RATIO ON ACOUSTIC-MODE INSTABILITY IN HYDROGEN-OXYGEN ROCKETS
260			_a _bNasa, Washington, D.C. _c1968
300			_a35
500			_aBound With Nasa Tn D-4731-32,4734-40
700			_aMorgan,C Joe
964			_gCIRC
997			_aTR14235 C
999			_c398653 _d398653