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Static Thrust Augmentation of a Rocket-Ejector System with a Heated Supersonic Primary JetStatic thrust augmentation of a rocket ejector system with a heated supersonic primary jet
Document ID
19620002195
Acquisition Source
Langley Research Center
Document Type
Other - NASA Technical Note (TN)
Authors
Simonson, Albert J. (NASA Langley Research Center Hampton, VA, United States)
Schmeer, James W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 1, 2013
Publication Date
May 1, 1962
Subject Category
Propellants
Report/Patent Number
NASA-TN-D-1261
Report Number: NASA-TN-D-1261
Accession Number
62N12195
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROCKET ENGINE
THRUST
EJECTOR
ROCKET
JET

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