000 00416pam a2200133a 44500
082 _aNASA
_bTN D-126
100 _aStein,Samuel
245 1 _aA HIGH-PERFORMANCE 250-POUND-THRUST ROCKET ENGINE UTILIZING GOAXIAL-FLOW INJECTION OF JP-4 FUEL AND LIQUID OXYGEN
260 _a
_bNasa, Washington, D.C.
_c1959
300 _a14
500 _aBound With Nasa Tn D-121-125,127-130
964 _gCIRC
997 _aTR15634 C
999 _c400582
_d400582