|
|
Scramjet Test Facility Operational Envelopes |
 |
|
|
||
Please note: These test envelopes have been constructed using an assumed forebody precompression and inviscid oblique shock theory to relate facility nozzle exit conditions to flight. Actual simulated flight conditions will vary depending upon test article design and installation details |
 Home
Other
Privacy Policy and Important Notices NASA Responsible Official: Edward G. Ruf Please send comments and questions regarding this site to: Site Curator Last updated: Monday, November 2, 2009 7:17 |