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Tether applicationsFor a range of tether lengths, end masses, and orbits, tether deployment concepts were defined and/or analyzed from the Orbiter for steady state/dynamic and up/down deployments and from circular/elliptical orbits. Orbits were defined and/or analyzed for end mass releasing concepts with steady state and dynamic releases taking into account tether and end mass motion before and after release. For a range of tether lengths, end masses, and orbits, tether retrieving or disposing concepts were defined and/or analyzed for both reusable and disposable tethers. Tether programs were installed or updated on the MSFC VAX 11/780 computer.
Document ID
19890001563
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 5, 2013
Publication Date
November 1, 1986
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:179392
NASA-CR-179392
Report Number: NAS 1.26:179392
Report Number: NASA-CR-179392
Accession Number
89N10934
Funding Number(s)
CONTRACT_GRANT: NAS8-35835
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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