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Future orbital transfer vehicle technology study. Volume 1: Executive summaryReusable space and ground based LO2/LH2 OTV's, both advanced space engines and aero assist capability were compared. The SB OTV provided advantages in life cycle cost, performance and potential for improvement. An all LO2/LH2 OTV fleet was also compared with a fleet of LO2/.H2 OTV's and electric OTV's. The normal growth technology electric OTV used silicon cells with heavy shielding and argon ion thrusters. In this case, the LO2/LH2 OTV fleet provided a 23% advantage in total transportation cost. An accelerated technology LF2/LH2 OTV provided improvements in performance relative to LO2/.H2 OTV but has higher DDT&E cost which negated its cost effectiveness. The accelerated technology electric vehicle used GaAs cells and annealing but still 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
19820017402
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
NASA-CR-3535-VOL-1
NAS 1.26:3535
Report Number: NASA-CR-3535-VOL-1
Report Number: NAS 1.26:3535
Accession Number
82N25278
Funding Number(s)
CONTRACT_GRANT: NAS1-16088
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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