Ionized plasma electromagnetic accelerators, noting thrust efficiency variation due to difference between supplied and expelled mass flow rate
Thrust efficiencies of electromagnetic engines.
1968-03-01
Sonstige
Keine Angabe
Englisch
Thrust efficiencies of electromagnetic engines.
AIAA | 1968
|Online Contents | 1996
NTIS | 1973
|Variable Thrust Rocket Engines
AIAA | 1960
|Gross thrust coefficient - Turbofan engines
AIAA | 1969
|