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Study of Plasma Motor Generator (PMG) tether system for orbit reboostA progress report is given on a system study by TRW begun in January 1987 of a 2 kW Plasma Motor Generator Tether to be used for orbit reboost. Following the completion of the initial phase in September 1987, additional tasks were agreed on and work on them begun in March 1988. These tasks fell into three categories: tests on the prototype tether fabricated during the first phase, simulations of the spacecraft and tether system after deployment using GTOSS, and a brief investigation of the impact and feasibility of increasing the system to 20 kW and hosting it on the Orbital Maneuvering Vehicle. The subcontractor, Energy Sciences Laboratory, was assigned the responsibility of performing the simulations and some mechanical tests on the prototype tether to supplement those done at TRW. A summary of the significant findings and issues from each task follows. Recommendations for future work constitutes the third section. A copy of the final briefing is in Appendix A, plus additional reports for each task and additional analysis.
Document ID
19880019565
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 5, 2013
Publication Date
June 1, 1988
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:172074
NASA-CR-172074
Report Number: NAS 1.26:172074
Report Number: NASA-CR-172074
Accession Number
88N28949
Funding Number(s)
PROJECT: RTOP 906-70-45-01
CONTRACT_GRANT: NAS9-17751
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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