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Aerobraked orbital transfer vehicle definitionA new technique has been developed to enhance the use of upper atmosphere aerobraking for increased performance from orbital transfer vehicles. This technique utilizes a pressure supported drag brake and the orbital transfer vehicle main engine to modulate aerodynamic drag and also to alleviate the aerodynamic heating during a grazing pass through the atmosphere. Performance analyses of vehicles utilizing all-propulsive or aerobraking during round trip missions from low earth orbit (LEO) to geo-synchronous earth orbit (GEO) and back shows that aerobraking allows a given vehicle to deliver approximately twice as much payload to GEO and return. Aerobraking also provides more than twice the round trip payload.
Document ID
19810036318
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Andrews, D. G.
(Boeing Co. Seattle, Wash., United States)
Bloetscher, F.
(Goodyear Aerospace Corp. Akron, Ohio, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1981
Subject Category
Astrodynamics
Report/Patent Number
AIAA PAPER 81-0279
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: St. Louis, MO
Start Date: January 12, 1981
End Date: January 15, 1981
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
81A20722
Funding Number(s)
CONTRACT_GRANT: NAS8-33532
Distribution Limits
Public
Copyright
Other

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