NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Heat-Pipe-Cooled Leading Edges for Hypersonic VehiclesHeat pipes can be used to effectively cool wing leading edges of hypersonic vehicles. . Heat-pipe leading edge development. Design validation heat pipe testing confirmed design. Three heat pipes embedded and tested in C/C. Single J-tube heat pipe fabricated and testing initiated. HPCLE work is currently underway at several locations.
Document ID
20080014285
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Glass, David E.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
July 12, 2006
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: Workshop on Materials and Structures for Hypersonic Flight
Location: Santa Barbara, CA
Country: United States
Start Date: July 12, 2006
End Date: July 13, 2006
Funding Number(s)
WBS: WBS 685771.01.049SY0.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available