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System design concepts and requirements for aeroassisted orbital transfer vehiclesThe Orbital Transfer Vehicle (OTV) is an advanced upper stage concept which will deliver spacecraft from operating systems at Low Earth Orbit (LEO) such as Space Shuttle, Earth-To-Orbit (ETO) vehicles, and Space Operations Center (SOC), to High Earth Orbit (HEO) and planetary excursions. The OTV will be driven by the need to achieve significant reductions in the operational costs for delivering payloads to Geostationary Equatorial Orbit (GEO). Aeroassist is a technological capability that has a potential for OTV's ranging from mission enhancing (reusable OTV for payload delivery) to mission enabling (manned GEO and some DOD). It is shown that the use of aeroassist for OTV's is a high leverage technology which can potentially reduce space transportation costs and enable a number of highly desirable missions.
Document ID
19820055603
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Austin, R. E.
(NASA Marshall Space Flight Center Advance Space Systems Group, Huntsville, AL, United States)
Cruz, M. I.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
French, J. R.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena CA, United States)
Date Acquired
August 10, 2013
Publication Date
August 1, 1982
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 82-1379
Meeting Information
Meeting: Atmospheric Flight Mechanics Conference
Location: San Diego, CA
Start Date: August 9, 1982
End Date: August 11, 1982
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
82A39138
Distribution Limits
Public
Copyright
Other

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