A supersonic combustion rocket is provided in which a small rocket motor is substituted for heavy turbo pumps in a conventional rocket engine. The substitution results in a substantial reduction in rocket engine weight. The flame emanating from the small rocket motor can act to ignite non-hypergolic fuels.
Supersonic-Combustion Rocket
1973
5 pages
Report
No indication
English
NTRS | 1973
|Air-Augmented Supersonic Rocket Combustion Booster
Online Contents | 1996
Analysis of a supersonic-combustion rocket concept
NTRS | 1972
|Analysis of a Supersonic-Combustion Rocket Concept
NTIS | 1972
|NTIS | 1975
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