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Operating characteristics of the Air Force Flight Dynamics Laboratory 50 megawatt hypersonic tests leg

Authors :
Beachler, J. C
Kachel, W. A
Source :
NASA. Goddard Space Flight Center Space Simulation.
Publication Year :
1972
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1972.

Abstract

A 50 megawatt hypersonic arc wind tunnel was developed, with up to 5.0-feet-diameter test sections, for thermostructural tests of lifting entry vehicles.

Subjects

Subjects :
Facilities, Research, And Support

Details

Language :
English
Database :
NASA Technical Reports
Journal :
NASA. Goddard Space Flight Center Space Simulation
Publication Type :
Report
Accession number :
edsnas.19720014642
Document Type :
Report

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