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Future orbital transfer vehicle technology study. Volume 2: Technical reportMissions for future orbit transfer vehicles (1995-2010) are identified and the technology, operations and vehicle concepts that satisfy the transportation requirements are defined. Comparison of reusable space and ground based LO2/LH2 OTV's was made. Both vehicles used advanced space engines and aero assist capability. The SB OTV provided advantages in life cycle cost, performance and potential for improvement. Comparison of an all LO2/LH2 OTV fleet with a fleet of LO2/LH2 OTVs and electric OTV's was also made. The normal growth technology electric OTV used silicon cells with heavy shielding and argon ion thrusters. This provided a 23% advantage in total transportation cost. The impact of accelerated technology was considered in terms of improvements in performance and cost effectiveness. The accelerated technology electric vehicle used GaAs cells and annealing but did not result in the mixed fleet being any cheaper than an all LO2/LH2 OTV fleet. It is concluded that reusable LO2/LH2 OTV's can serve all general purpose cargo roles between LEO and GEO for the forseeable future. The most significant technology for the second generation vehicle would be space debris protection, on-orbit propellant storage and transfer and on-orbit maintenance capability.
Document ID
19820016399
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Davis, E. E.
(Boeing Aerospace Co. Seattle, WA, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1982
Publication Information
Publisher: NASA
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NAS 1.26:3536
NASA-CR-3536
Accession Number
82N24275
Funding Number(s)
CONTRACT_GRANT: NAS1-16088
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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