Space shuttle base heating tests were conducted using a 0.040-scale model in the Plum Brook Space Power Facility of The NASA Lewis Research Center. The tests measured heat transfer rates, pressure distributions, and gas recovery temperatures on the orbiter vehicle 2A base configuration resulting from engine plume impingement. One hundred and sixty-eight hydrogen-oxygen engine firings were made at simulated flight altitudes ranging from 120,000 to 360,000 feet. (Author)
The 0.040-Scale Space Shuttle Orbiter Base Heating Model Tests in the Lewis Research Center Space Power Facility
1976
44 pages
Report
Keine Angabe
Englisch
Space Shuttle Orbiter Barricade
NTIS | 1974
|Space shuttle orbiter avionics
Tema Archiv | 1977
|NTRS | 2001
NTIS | 1994