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Ten-millipound resistojet performance.Design, fabrication and performance of 10- millipound resistojet operating on hydrogen or ammonia, describing heat exchanger and nozzle geometry
Document ID
19670059970
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Page, R. J.
Short, R. A.
Date Acquired
August 3, 2013
Publication Date
September 1, 1967
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 67-664
Report Number: AIAA PAPER 67-664
Accession Number
67A38699
Funding Number(s)
CONTRACT_GRANT: NAS1-6702
Distribution Limits
Public
Copyright
Other
Keywords
RESISTOJET ENGINE
NOZZLE GEOMETRY
HEAT EXCHANGER
SPACECRAFT PERFORMANCE
ENGINE DESIGN

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