COMBUSTION AND PROPULSIVE CHARACTERISTICS OF POTENTIAL HYBRID ROCKET PROPELLANT
IAF Space Propulsion Symposium ; 2019 ; Washington, DC
2020
Aufsatz (Konferenz)
Englisch
Propulsive potential of residual rocket motor heat
NTRS | 1968
|Propulsive Potential of Residual Rocket Motor Heat
NTIS | 1968
|Advantages of higher combustion velocities in rocket propulsive charges
Engineering Index Backfile | 1966
|Liquid propellant rocket combustion instability
TIBKAT | 1972
|Combustion in solid-propellant rocket engines
NTRS | 1968
|