NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Active cooling from the sixties to NASPVehicles, such as the X-15 or National Aero-Space Plane, 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 this 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--are described. Many of the lessons learned from these research efforts are presented.
Document ID
19930003270
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kelly, H. Neale
(NASA Langley Research Center Hampton, VA, United States)
Blosser, Max L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1992
Publication Information
Publication: Current Technology for Thermal Protection Systems
Subject Category
Aircraft Design, Testing And Performance
Accession Number
93N12458
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available