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
Instrumentation design study for testing a hypersonic ramjet engine on the x-15 a-2. volume 2- preliminary design of in-flight thrust/drag measuring deviceInflight thrust and drag measuring device for hypersonic ramjet engine on X-15A-2 aircraft
Document ID
19650011863
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Demichele, D. J. (General Electric Co. Cincinnati, OH, United States)
George, R. L. (General Electric Co. Cincinnati, OH, United States)
Mains, R. M. (General Electric Co. Cincinnati, OH, United States)
Wood, N. H. (General Electric Co. Cincinnati, OH, United States)
Date Acquired
August 2, 2013
Publication Date
March 1, 1965
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-CR-62183
Report Number: NASA-CR-62183
Accession Number
65N21464
Funding Number(s)
CONTRACT_GRANT: NAS4-715
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
X-15 AIRCRAFT
RAMJET ENGINE
THRUST MEASUREMENT
DRAG MEASUREMENT

Related Records

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