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Flight Reentry ExperimentsReentry technology has long depended on the simulation provided by wind tunnels, shock tubes, arc jets, and a variety of other ground facilities to advance the experimental verification of the results predicted from theory or postulated empirically from previous tests. As the application of information thus obtained approaches the point of application to the design of flight systems, the question of the extent to which the information can he applied with confidence inevitably arises. Sources of uncertainty are the assumptions necessary to obtain theoretical solutions, the inadequacy with which the complex reentry environment can be totally simulated on the ground, and the question of how well the ground facility results have been validated by flight comparisons. Thus the value of flight reentry testing is greatest when the tests either explore the nature of a phenomenon, difficult or impossible to simulate on the ground, or provide the validation for use of a system or concept developed from ground-based research.
Document ID
19690009639
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Herbert A Wilson, Jr
(Langley Research Center Hampton, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1964
Publication Information
Publication: Proceedings of the Conference on the Role of Simulation in Space Technology, Part B
Publisher: National Aeronautics and Space Administration
Subject Category
Ground Support Systems and Facilities (Space)
Report/Patent Number
NASA-CR-64950
NASA-CR-100138
Meeting Information
Meeting: Conference on the Role of Simulation in Space Technology
Location: Blacksburg, VA
Country: US
Start Date: August 17, 1964
End Date: August 21, 1964
Sponsors: National Aeronautics and Space Administration
Accession Number
69N18977
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
Reentry Effect
Flight Test
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