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Thermal-structural test facilities at NASA DrydenThe National Aero-Space Plane (NASP) has renewed interest in hypersonic flight and hot-structures technology development for both the airframe and engine. The NASA Dryden Thermostructures Research Facility is a unique national facility that was designed to conduct thermal-mechanical tests on aircraft and aircraft components by simulating the flight thermal environment in the laboratory. The layout of the facility is presented, which includes descriptions of the high-bay test area, the instrumentation laboratories, the mechanical loading systems, and the state-of-the-art closed-loop thermal control system. The hot-structures test capability of the facility is emphasized by the Mach-3 thermal simulation conducted on the YF-12 airplane. The Liquid-Hydrogen Structural Test Facility, which is presently in the design phase, will provide the capability of thermally testing structures containing hydrogen.
Document ID
19920024958
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Deangelis, V. Michael
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Anderson, Karl F.
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1992
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
H-1818
NAS 1.15:104249
NASA-TM-104249
Report Number: H-1818
Report Number: NAS 1.15:104249
Report Number: NASA-TM-104249
Meeting Information
Meeting: Annual Society for Flight Test Engineers Symposium
Location: Hauppauge, NY
Country: United States
Start Date: August 3, 1992
End Date: August 6, 1992
Accession Number
92N34202
Funding Number(s)
PROJECT: RTOP 505-62-40
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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