Potential Benefits of Pressure Gain Combustion in Liquid Rocket Engine Pre-Burners
51st AIAA/SAE/ASEE Joint Propulsion Conference
01.01.2015
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Potential Benefits of Pressure Gain Combustion in Liquid Rocket Engine Pre-Burners (AIAA 2015-3762)
British Library Conference Proceedings | 2015
|Liquid rocket engine combustion instability
TIBKAT | 1995
|Burners for Disposal of Rocket Propellants
NTIS | 1976
|