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The flight demonstration program and selection processThe Orbital Refueling System (ORS); force torque sensor; Plasma Motor/Generator (PMG) proof of function; voice controlled system; infrared intercommunications; superfluid helium on orbit transfer; laser docking sensor; and the Small Expendable Deployment System (SEDS) are summarized.
Document ID
19880001489
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Levin, G. M. (NASA Headquarters Washington, DC United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1987
Publication Information
Publication: NASA. Langley Research Center, Hampton, Va. Space Construction
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
88N10871
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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