The concept of the effective ejection velocity of a rocket engine is explained and the magnitude of the attainable ejection velocity theoretically and experimentally investigated. Velocities above 3000 meters per second (6700 mph) are actually measured and the possibilities of further increases shown.
Recent Results in Rocket Flight Technique
1942-04-01
Miscellaneous
No indication
English
Recent results in rocket flight technique
Engineering Index Backfile | 1942
|VEGA Solid Rocket Motors Flight Performances results
AIAA | 2013
|Springer Verlag | 2018
|Results from sert i ion rocket flight test
NTRS | 1965
|Results from Sert I Ion Rocket Flight Test
NTIS | 1965
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