COMBUSTION AND PROPULSIVE CHARACTERISTICS OF POTENTIAL HYBRID ROCKET PROPELLANT
IAF Space Propulsion Symposium ; 2019 ; Washington, DC
2020
Conference paper
English
Propulsive Potential of Residual Rocket Motor Heat
NTIS | 1968
|Liquid propellant rocket combustion instability
TIBKAT | 1972
|Liquid propellant rocket combustion instability
NTRS | 1972
|Liquid Propellant Rocket Combustion Instability
NTIS | 1972
|Combustion in solid-propellant rocket engines
NTRS | 1968
|