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Benefits of high aerodynamic efficiency to orbital transfer vehiclesThe benefits and costs of high aerodynamic efficiency on aeroassisted orbital transfer vehicles (AOTV) are analyzed. Results show that a high lift to drag (L/D) AOTV can achieve significant velocity savings relative to low L/D aerobraked OTV's when traveling round trip between low Earth orbits (LEO) and alternate orbits as high as geosynchronous Earth orbit (GEO). Trajectory analysis is used to show the impact of thermal protection system technology and the importance of lift loading coefficient on vehicle performance. The possible improvements in AOTV subsystem technologies are assessed and their impact on vehicle inert weight and performance noted. Finally, the performance of high L/D AOTV concepts is compared with the performances of low L/D aeroassisted and all propulsive OTV concepts to assess the benefits of aerodynamic efficiency on this class of vehicle.
Document ID
19850008687
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Andrews, D. G.
(Boeing Co. Seattle, WA, United States)
Norris, R. B.
(Air Force Wright Aeronautical Labs. Seattle, WA, United States)
Paris, S. W.
(Boeing Co.)
Date Acquired
August 12, 2013
Publication Date
April 1, 1984
Publication Information
Publication: NASA. Lewis Research Center OTV Propulsion Issues
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
85N16996
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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