Interim summary of liquid rocket acoustic-mode-instability studies at a nominal thrust of 20 000 pounds
NASA technical note ; D-4968
1969
90 S
Report
Englisch
Acoustic Mode Analysis of Rocket Thrust Chambers
AIAA | 2019
|Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust
SAE Technical Papers | 2000