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Electric Propulsion Orbital PlatformThis paper describes the Electric Propulsion Orbital Platform (EPOP), of which the primary objective is to provide an instrumented platform for testing electric propulsion devices in space. It is anticipated that the first flight, EPOP-1, will take place on the Shuttle-deployed Wake Shield Facility in 1996, and will be designed around a commercial 1.8 kW arcjet system which will be operated on gaseous hydrogen propellant. Specific subsystems are described, including the arcjet system, the propellant and power systems, and the diagnostics systems.
Document ID
19960009788
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
V. J. Friedly (Tennessee Univ. - Calspan Tullahoma, TN, United States)
Wilhelmus M. Ruyten (Tennessee Univ. - Calspan Tullahoma, TN, United States)
R. J. Litchford (Tennessee Univ. - Calspan Tullahoma, TN, United States)
G. W. Garrison (Tennessee Univ. - Calspan Tullahoma, TN, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1993
Publication Information
Publication: Center for Space Transportation and Applied Research Fifth Annual Technical Symposium Proceedings
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-199696
NIPS-96-05977
NAS 1.26:199696
Meeting Information
Meeting: The Fifth Annual Technical Symposium
Location: Tullahoma, TN
Country: US
Start Date: November 9, 1993
Sponsors: University of Tennessee Space Institute
Accession Number
96N16954
Funding Number(s)
CONTRACT_GRANT: NAGW-1195
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19960009774Collected WorksCenter for Space Transportation and Applied Research Fifth Annual Technical Symposium Proceedings
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