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Theoretical analyses of electrothermal thrusters with supersonic heat additionTheoretical performance analyses for electrothermal thrustor using lithium propellant with combination of radioisotope and electrical energy sources
Document ID
19700006928
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Leon, H. I. (Colorado State Univ. Fort Collins, CO, United States)
Mickelsen, W. R. (Colorado State Univ. Fort Collins, CO, United States)
Date Acquired
August 6, 2013
Publication Date
May 1, 1969
Publication Information
Publication: ADVANCED ELEC. PROPULSION RES. MAY 1969 (SEE N70-16231 05-28)
Subject Category
Propulsion Systems
Meeting Information
Meeting: AIAA 7TH ELEC. PROPULSION CONF.
Location: WILLIAMSBURG, VA
Country: UNITED STATES
Start Date: March 3, 1969
End Date: March 5, 1969
Accession Number
70N16232
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitleCollected Works19700006927Collected WorksAdvanced Electric Propulsion Research Final Report, 1 Jul. - 31 Dec. 196819700006927Collected WorksAdvanced Electric Propulsion Research Final Report, 1 Jul. - 31 Dec. 1968N70-16231 05-28Collected Works
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