NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Hyper-X Hot Structures Comparison of Thermal Analysis and Flight DataThe Hyper-X (X-43A) program is a flight experiment to demonstrate scramjet performance and operability under controlled powered free-flight conditions at Mach 7 and 10. The Mach 7 flight was successfully completed on March 27, 2004. Thermocouple instrumentation in the hot structures (nose, horizontal tail, and vertical tail) recorded the flight thermal response of these components. Preflight thermal analysis was performed for design and risk assessment purposes. This paper will present a comparison of the preflight thermal analysis and the recorded flight data.
Document ID
20040111308
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Amundsen, Ruth M.
(NASA Langley Research Center Hampton, VA, United States)
Leonard, Charles P.
(NASA Langley Research Center Hampton, VA, United States)
Bruce, Walter E., III
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
Paper 109-A0016
Report Number: Paper 109-A0016
Meeting Information
Meeting: Fifteenth Annual Thermal and Fluids Analysis Workshop
Location: Pasadena, CA
Country: United States
Start Date: August 29, 2004
End Date: September 3, 2004
Funding Number(s)
OTHER: 23-745-30-20
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available