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Tether Transportation System StudyThe projected traffic to geostationary earth orbit (GEO) is expected to increase over the next few decades. At the same time, the cost of delivering payloads from the Earth's surface to low earth orbit (LEO) is projected to decrease, thanks in part to the Reusable Launch Vehicle (RLV). A comparable reduction in the cost of delivering payloads from LEO to GEO is sought. The use of in-space tethers, eliminating the requirement for traditional chemical upper stages and thereby reducing the launch mass, has been identified as such an alternative. Spinning tethers are excellent kinetic energy storage devices for providing the large delta vee's required for LEO to GEO transfer. A single-stage system for transferring payloads from LEO to GEO was proposed some years ago. The study results presented here contain the first detailed analyses of this proposal, its extension to a two-stage system, and the likely implementation of the operational system.
Document ID
19980048417
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Publication (TP)
Authors
Bangham, M. E.
(Boeing Co. Huntsville, AL United States)
Lorenzini, E.
(Smithsonian Astrophysical Observatory Cambridge, MA United States)
Vestal, L.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1998
Subject Category
Astronautics (General)
Report/Patent Number
NASA/TP-1998-206959
M-853
NAS 1.60:206959
Funding Number(s)
CONTRACT_GRANT: NAS8-39400
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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