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Heat transfer tests on a 0.01-scale rockwell configuration 3 space shuttle orbiter and tank (37-ot) in the calspan 48-inch hypersonic shock tunnel (oh12/ih21), volume 3
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kotch, M. |
| Copyright Year | 1975 |
| Description | Tabulated source data are presented for wind tunnel tests conducted on scale models of the space shuttle orbiter and external tank. |
| File Size | 24376829 |
| Page Count | 569 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760009055 |
| Archival Resource Key | ark:/13960/t7sn4zr9q |
| Language | English |
| Publisher Date | 1975-10-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Tables Data External Tanks Hypersonic Speed Scale Models Aerodynamic Heat Transfer Reynolds Number Reentry Trajectories Wind Tunnel Tests Hypersonic Heat Transfer Angle of Attack Space Shuttle Orbiters Shock Tunnels 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 |