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Space Station Freedom assembly and operation at a 51.6 degree inclination orbitThis study examines the implications of assembling and operating Space Station Freedom at a 51.6 degree inclination orbit utilizing an enhanced lift Space Shuttle. Freedom assembly is currently baselined at a 220 nautical mile high, 28.5 degree inclination orbit. Some of the reasons for increasing the orbital inclination are (1) increased ground coverage for Earth observations, (2) greater accessibility from Russian and other international launch sites, and (3) increased number of Assured Crew Return Vehicle (ACRV) landing sites. Previous studies have looked at assembling Freedom at a higher inclination using both medium and heavy lift expendable launch vehicles (such as Shuttle-C and Energia). The study assumes that the shuttle is used exclusively for delivering the station to orbit and that it can gain additional payload capability from design changes such as a lighter external tank that somewhat offsets the performance decrease that occurs when the shuttle is launched to a 51.6 degree inclination orbit.
Document ID
19930015985
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Troutman, Patrick A.
(NASA Langley Research Center Hampton, VA, United States)
Brewer, Laura M.
(Analytical Mechanics Associates, Inc. Hampton, VA., United States)
Heck, Michael L.
(Analytical Mechanics Associates, Inc. Hampton, VA., United States)
Kumar, Renjith R.
(Analytical Mechanics Associates, Inc. Hampton, VA., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1993
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TM-107731
NAS 1.15:107731
Report Number: NASA-TM-107731
Report Number: NAS 1.15:107731
Accession Number
93N25174
Funding Number(s)
PROJECT: RTOP 476-14-15-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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