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Resistojet propulsion for large spacecraft systemsResistojet propulsion systems have characteristics that are ideally suited for the on-orbit and primary propulsion requirements of large spacecraft systems. These characteristics which offer advantages over other forms of propulsion are reviewed and presented. The feasibility of resistojets were demonstrated in space whereas only a limited number of ground life tests were performed. The major technology issues associated with these ground tests are evaluated. The past performance of resistojets is summarized and, looks into the present day technology status is reviewed. The material criteria, along with possible concepts, needed to attain high performance resistojets are presented.
Document ID
19840003138
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mirtich, M. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-TM-83489
NAS 1.15:83489
E-1813
Meeting Information
Meeting: Intern. Elec. Propulsion Conference
Location: New Orleans, LA
Country: United States
Start Date: November 17, 1982
End Date: November 19, 1982
Sponsors: Deutsche Gesselschaft fur Luft-und Raumfarhrt, AIAA, Japan Soc. for Aeron. and Space Sci.
Accession Number
84N11206
Funding Number(s)
PROJECT: RTOP 506-55-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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