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Geostationary platform systems concepts definition study. Volume 2: Technical, book 2A selected concept for a geostationary platform is defined in sufficient detail to identify requirements for supporting research and technology, space demonstrations, GFE interfaces, costs, and schedules. This system consists of six platforms in geostationary orbit (GEO) over the Western Hemisphere and six over the Atlantic, to satisfy the total payload set associated with the nominal traffic model. Each platform is delivered to low Earth orbit (LEO) in a single shuttle flight, already mated to its LEO to GEO transfer vehicle and ready for deployment and transfer to GEO. An alternative concept is looked at briefly for comparison of configuration and technology requirements. This alternative consists of two large platforms, one over the Western Hemisphere consisting of three docked modules, and one over the Atlantic (two docked modules), to satisfy a high traffic model. The modules are full length orbiter cargo bay payloads, mated at LEO to orbital transfer vehicles (OTVs) delivered in other shuttle flights, for transfer to GEO, rendezvous, and docking. A preliminary feasibility study of an experimental platform is also performed to demonstrate communications and platform technologies required for the operational platforms of the 1990s.
Document ID
19810009550
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 4, 2013
Publication Date
June 1, 1980
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
GDC-GPP-79-006-VOL-2-BK-2
NASA-CR-161649
Report Number: GDC-GPP-79-006-VOL-2-BK-2
Report Number: NASA-CR-161649
Accession Number
81N18074
Funding Number(s)
CONTRACT_GRANT: NAS8-33527
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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