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3 kw concentric tubular resistojet performance compared with theory.Resistojet design and fabrication, using hydrogen propellant and having 3-kw power input
Document ID
19660042161
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Halbach, C. R.
Page, R. J.
Short, R. A.
Date Acquired
August 3, 2013
Publication Date
March 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 66-224
Report Number: AIAA PAPER 66-224
Accession Number
66A21451
Funding Number(s)
CONTRACT_GRANT: NASW-1070
Distribution Limits
Public
Copyright
Other
Keywords
ENGINE DESIGN
HYDROGEN FUEL
RESISTOJET ENGINE
PROPULSIVE EFFICIENCY

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