An Experimental Evaluation of 100-Lb-Thrust Ablatively Cooled Rocket Engines
1966
35 pages
Report
No indication
English
Rocket Engines & Motors , Ablation , Rocket chamber , Test firing , Bipropellant , Carbide , Chamber , Combustion , Firing , Insert , Liquid , Molybdenum , Silicon , Throat , Thrust
Ablatively cooled pulse rocket engine design
AIAA | 1964
|Ablatively cooled pulse rocket engine design
AIAA | 1965
|