The present invention relates to improved rocket engine systems. In one embodiment, an improved rocket engine system includes a propellant source, at least one power source, at least one power source motor, a rocket engine, and at least one pump. The improved rocket engine system may further include at least one of the following: at least one controller, at least one propellant valve, and a propellant pressurizing source.
Rocket Engines Systems
2018-05-10
Patent
Elektronische Ressource
Englisch
NTIS | 1976
|NTIS | 1968
|Engineering Index Backfile | 1957
|NTIS | 1969
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