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Test facilities for high power electric propulsionElectric propulsion has applications for orbit raising, maneuvering of large space systems, and interplanetary missions. These missions involve propulsion power levels from tenths to tens of megawatts, depending upon the application. General facility requirements for testing high power electric propulsion at the component and thrust systems level are defined. The characteristics and pumping capabilities of many large vacuum chambers in the United States are reviewed and compared with the requirements for high power electric propulsion testing.
Document ID
19920001918
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sovey, James S.
(Sverdrup Technology, Inc., Brook Park OH., United States)
Vetrone, Robert H.
(NASA Lewis Research Center Cleveland, OH, United States)
Grisnik, Stanley P.
(NASA Lewis Research Center Cleveland, OH, United States)
Myers, Roger M.
(NASA Lewis Research Center Cleveland, OH, United States)
Parkes, James E.
(Sverdrup Technology, Inc., Brook Park OH., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-TM-105247
NAS 1.15:105247
AIAA PAPER 91-3499
E-6576
Report Number: NASA-TM-105247
Report Number: NAS 1.15:105247
Report Number: AIAA PAPER 91-3499
Report Number: E-6576
Meeting Information
Meeting: Conference on Advanced Space Exploration Initiative Technologies
Location: Cleveland, OH
Country: United States
Start Date: September 4, 1991
End Date: September 6, 1991
Sponsors: AIAA, OAI, NASA
Accession Number
92N11136
Funding Number(s)
PROJECT: RTOP 506-42-31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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