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
Wind-tunnel force and pressure tests of rocket-engine nozzle extensions on the 0.0667-scale X-15-2 model at supersonic and hypersonic speedsWind tunnel force and pressure tests of rocket engine nozzle extensions on X-15-2 model at supersonic and hypersonic speeds
Document ID
19690011511
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Montoya, E. J. (NASA Flight Research Center Edwards, CA, United States)
Nugent, J. (NASA Flight Research Center Edwards, CA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1969
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-1759
Report Number: NASA-TM-X-1759
Accession Number
69N20873
Funding Number(s)
CONTRACT_GRANT: 729-00-00-01-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

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