000			00480pam a2200133a 44500
082			_aNASA _bTN D-129
100			_aHersch,Martin
245	1		_aCOMBINED EFFECT OF CONTRACTION RATIO AND CHAMBER PRESSURE ON THE PERFORMANCE OF A GASEOUS-HYDROGEN-LIQUID-OXYGEN COMBUSTOR FOR A GIVEN PROPELLANT WEIGHT FLOW AND OXIDANT-FUEL RATIO
260			_a _bNasa, Washington, D.C. _c1961
300			_a13
500			_aBound With Nasa Tn D-121-128,130
964			_gCIRC
997			_aTR15637 C
999			_c400585 _d400585