Liquid rocket acoustic instability for hydrogen-oxygen and earth storable propellant combinations
Liquid rocket acoustic-mode-instability studies at a nominal thrust of 20000 pounds
1968-12-01
Sonstige
Keine Angabe
Englisch
Acoustic Mode Analysis of Rocket Thrust Chambers
AIAA | 2019
|Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust
SAE Technical Papers | 2000