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Recent Results in Rocket Flight TechniqueThe 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.
Document ID
19930094405
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Sanger, Eugen
Date Acquired
September 6, 2013
Publication Date
April 1, 1942
Report/Patent Number
NACA-TM-1012
Accession Number
93R23325
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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