The liquid propellant rocket engine is for manned aircraft and spacecraft. The engine maintains a constant combustion chamber pressure during throttling at high or low altitudes. The engine has a pintle for varying the exhaust throat area which may be inclined to deflect the exhaust gases for steering purposes.
Variable Thrust Rocket Engine Incorporating Thrust Vector Control
1965
1 pages
Report
Keine Angabe
Englisch
Toward variable-thrust liquid-rocket engine
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