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The next generation of reentry vehicles: NASA's viewThe term reentry vehicle is used in the broad sense. The vehicles addressed include not only those that return from orbit to the Earth's surface, but also aeroassisted orbit transfer vehicles that use aerodynamic forces generated during atmospheric passes to achieve orbital changes with a smaller expenditure of energy than is required for an all-propulsion vehicle. Advanced reusable launch vehicles with special emphasis on system concepts and the influence of advanced technology on entry vehicle configuration are considered. Three categories of orbital transfer vehicles discussed: synergetic plane-change vehicles, planetary aerocapture vehicles, and LEO to GEO orbital transfer vehicles. While the orbital transfer and planetary vehicles are quite different from conventional winged Earth entry vehicles, synergetic plane change and high cross-range Earth entry vehicles have many similarities. Finally, a possible scenario for the development of the next generation of reentry vehicles is presented.
Document ID
19840017590
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Walberg, G. D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Publication Information
Publication: Von Karman Inst. for Fluid Dynamics Hypersonic Aerothermodyn.
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
84N25658
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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