Loading...
Please wait, while we are loading the content...
Similar Documents
Results of an investigation of the 0.003-scale space shuttle external tank msfc model 460 in the nasa/msfc 14 x 14 inch trisonic wind tunnel to determine static pressure distributions during reentry (ta2f), volume 3
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Ramsey, P. E. Winkler, G. W. |
| Copyright Year | 1975 |
| Description | Static pressure distributions for the external tank (ET) at reentry conditions are presented. Basic configuration of the model was the MCR 0200 ET modified to include a rectangular crossbar at the aft ET/orbiter attach point. Mach numbers were 1.96, 3.48, and 4.96. Reynolds number per foot at these Mach numbers were 6.95 million, 6.42 million, and 4.95 million, respectively. Angle of attack range was -8 to 100 degrees and roll angle was 0 to 315 degrees. |
| File Size | 27135901 |
| Page Count | 856 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760009067 |
| Archival Resource Key | ark:/13960/t3vt6f263 |
| Language | English |
| Publisher Date | 1975-11-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Static Pressure External Tanks Reentry Effects Aerodynamic Configurations Supersonic Speed Scale Models Space Shuttles Wind Tunnel Tests Pressure Distribution Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
