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Theoretical analyses of electrothermal thrusters with supersonic heat additionPerformance analysis for electrothermal thrustor using lithium propellant with supersonic heat addition
Document ID
19700041043
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Leon, H. I.
Mickelsen, W. R.
Date Acquired
August 5, 2013
Publication Date
December 1, 1969
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 69-286
Report Number: AIAA PAPER 69-286
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, ELECTRIC PROPULSION CONFERENCE, 7TH
Location: WILLIAMSBURG, VA
Start Date: March 3, 1969
End Date: March 5, 1969
Sponsors: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
70A17159
Funding Number(s)
CONTRACT_GRANT: NGR-06-002-032
Distribution Limits
Public
Copyright
Other

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