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Experimental performance of a high specific impulse arc jet engine.Liquid cooled high specific impulse arc jet engine has measured engine thrust not completely aerodynamic in nature
Document ID
19660048180
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Bennett, S.
Connors, J. F.
John, R. R.
Date Acquired
August 3, 2013
Publication Date
April 1, 1965
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 64-669
Report Number: AIAA PAPER 64-669
Accession Number
66A27470
Funding Number(s)
CONTRACT_GRANT: NAS3-2593
Distribution Limits
Public
Copyright
Other
Keywords
ARC JET
JET ENGINE
SPECIFIC IMPULSE
PLASMA ENGINE
PROPULSIVE EFFICIENCY

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