NASA / TN D-129
Hersch,Martin
       COMBINED 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 / .- Nasa, Washington, D.C., 1961 .- 13 .
Bound With Nasa Tn D-121-128,130
Copy Details:
Acc. No.: TR15637, Full Call No.: NASA TN D-129, Item type: Technical Report , Location: General Stacks,
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