The effect of momentum ratio on dome overheating for a throttleable bipropellant rocket engine
29th Aerospace Sciences Meeting ; 1991 ; Reno , NV , U.S.A.
01.01.1991
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
AXISYMMETRIC, THROTTLEABLE NON-GIMBALLED ROCKET ENGINE
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