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SCALE MODEL TESTING OF 90 DEG TURN EJECTOR SYSTEMS FOR ROCKET ENGINE ALTITUDE SIMULATIONScale model testing of 90 degree turn ejector systems for rocket engine altitude simulation
Document ID
19630022693
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Mandell, B.
Mc Farland, B. L.
Nelson, R. E.
Patmor, G. O.
Date Acquired
August 1, 2013
Publication Date
June 20, 1963
Subject Category
Aircraft
Report/Patent Number
AIAA PAPER 63-174
Report Number: AIAA PAPER 63-174
Accession Number
63A18752
Funding Number(s)
CONTRACT_GRANT: SF-4756
CONTRACT_GRANT: AT/29-2/-1060
Distribution Limits
Public
Copyright
Other
Keywords
NUCLEAR ROCKET
ALTITUDE SIMULATION
ROCKET ENGINE

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