NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
SCALE MODEL TESTING OF 90 DEG TURN EJECTOR SYSTEMS FOR ROCKET ENGINE ALTITUDE SIMULATIONScale model testing of 90-deg turn ejector systems for rocket engine simulation
Document ID
19630007926
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mandell, B. (Aerojet-General Corp. Azusa, CA, United States)
Mc Farland, B. L. (Aerojet-General Corp. Azusa, CA, United States)
Nelson, R. E. (Aerojet-General Corp. Azusa, CA, United States)
Patmor, G. O. (Aerojet-General Corp. Azusa, CA, United States)
Date Acquired
August 1, 2013
Publication Date
January 1, 1963
Subject Category
Aircraft
Report/Patent Number
AIAA PAPER-63-174
Report Number: AIAA PAPER-63-174
Accession Number
63N17802
Funding Number(s)
CONTRACT_GRANT: AT/29-2/-1060
CONTRACT_GRANT: SNP-1
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROCKET ENGINE
ALTITUDE SIMULATION
EJECTOR
Document Inquiry

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available