000 00517pam a2200145a 44500
082 _aNASA
_bTN D-4392 -
100 _aStabe,Roy G
245 1 _aCOLD-AIR PERFORMANCE EVALUATION OF SCALE MODEL OXIDIZER PUMP-DRIVE TURBINE FOR THE M-1 HYDROGEN-OXYGEN ROCKET ENGINE
_bIII - PERFORMANCE OF FIRST STAGE WITH INLET-FEEDPIPE- MANIFOLD ASSEMBLY
260 _a
_bNasa, Washington, D.C.
_c1968
300 _a20
500 _aBound With Nasa Tn D-4391-4400
700 _aKline,John F
964 _gCIRC
997 _aTR10261 C
999 _c394427
_d394427