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Definition of an entry research vehicleWithin the last year, there has been a growing interest in technology which would support the development of vehicles which can maneuver in the atmosphere while returning from orbit and vehicles which can fly in the atmosphere at hypersonic speeds for sustained periods of time. This rebirth of interest in hypersonics is partly a result of a developing awareness of the potential benefits which can be derived from vehicles with capability to operate between the limits of existing aircraft and spacecraft. Examples of the types of maneuvers which are projected for this new class of vehicles are presented. Challenges provided by the considered maneuvers are summarized, taking into account a synergetic or atmospheric plane change. The plane change maneuver will require a Thermal Protection System (TPS). Attention is given to the definition of a Shuttle launched entry research vehicle experiment. Details regarding the synergetic plane change are considered along with the maneuvering entry, vehicle heating, and experiments and instrumentation.
Document ID
19850056793
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Freeman, D. C.
(NASA Langley Research Center Hampton, VA, United States)
Powell, R. W.
(NASA Langley Research Center Hampton, VA, United States)
Naftel, J. C.
(NASA Langley Research Center Hampton, VA, United States)
Wurster, K. E.
(NASA Langley Research Center Space Systems Div., Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1985
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 85-0969
Accession Number
85A38944
Distribution Limits
Public
Copyright
Other

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