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Active cooling from the sixties to NASPVehicles, such as the X-15 or the National Aerospace Plane (NASP), traveling at hypersonic speeds through the earth's atmosphere experience aerodynamic heating. The heating can be severe enough that a thermal protection system is required to limit the temperature of the vehicle structure. Although several categories of thermal protection systems are mentioned briefly, the majority of the present paper describes convectively cooled structures for large areas. Convective cooling is a method of limiting structural temperatures by circulating a coolant through the vehicle structure. Efforts to develop convectively cooled structures during the past 30 years, from early engine structures which were intended to be tested on the X-15 to structural panels fabricated and tested under the NASP program, are described. Many of the lessons learned from these research efforts are presented.
Document ID
19940033030
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kelly, H. Neale
(Analytical Services and Materials, Inc. Hampton, VA., United States)
Blosser, Max L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1994
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-109079
NAS 1.15:109079
Report Number: NASA-TM-109079
Report Number: NAS 1.15:109079
Meeting Information
Meeting: Current Technology for Thermal Protection Systems Workshop
Location: Hampton, VA
Country: United States
Start Date: February 11, 1992
End Date: February 12, 1992
Accession Number
94N37541
Funding Number(s)
PROJECT: RTOP 505-70-63-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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