Performance of a hypersonic hot fuselage structure with a carbon dioxide frost protected, nonintegral cryogenic tank
Title:
Performance of a hypersonic hot fuselage structure with a carbon dioxide frost protected, nonintegral cryogenic tank
Author:
Sharpe, Ellsworth L.
Personal Author:
Publication Information:
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va.] : [For sale by the National Technical Information Service], 1975.
Physical Description:
48 pages : illustrations ; 27 cm.
General Note:
Cover title.
Prepared at Langley Research Center.
Language:
English
Added Author:
Added Corporate Author:
Format :
Book