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The ballistic range and aerothermodynamic testingA renewed interest in hypervelocity vehicles requires an increase in our knowledge of aerothermodynamic phenomena. Tests conducted in our ground-based facilities can be used both to better understand the physics of hypervelocity flight, and to calibrate and validate computer codes designed to predict vehicle performance in the hypervelocity environment. This paper reviews the requirements for aerothermodynamic testing and discusses the ballistic range and its capabilities. Examples of the kinds of testing performed in typical high-performance ballistic ranges are described; we draw heavily on experience obtained in the ballistics facilities at NASA Ames. Prospects for improving the capabilities of the ballistic range by using advanced instrumentation are discussed. Finally, recent developments in gun technology and their application to extend the capability of the ballistic range are summarized.
Document ID
19880050696
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Strawa, A. W.
(NASA Ames Research Center Moffett Field, CA, United States)
Chapman, G. T.
(NASA Ames Research Center Moffett Field, CA, United States)
Arnold, J. O.
(NASA Ames Research Center Moffett Field, CA, United States)
Canning, T. N.
(Eloret Institute Sunnyvale, CA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Ground Support Systems And Facilities (Space)
Report/Patent Number
AIAA PAPER 88-2015
Report Number: AIAA PAPER 88-2015
Meeting Information
Meeting: Aerodynamic Testing Conference
Location: San Diego, CA
Country: United States
Start Date: May 18, 1988
End Date: May 20, 1988
Sponsors: AIAA
Accession Number
88A37923
Funding Number(s)
CONTRACT_GRANT: NCC2-504
Distribution Limits
Public
Copyright
Other

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