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Exploratory study of performance of the langley pilot model expansion tube with a hydrogen driver
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1966 |
| Description | Expansion tube for simulating hypervelocity flow conditions for reentry vehicles |
| File Size | 2211888 |
| Page Count | 50 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19660015871 |
| Archival Resource Key | ark:/13960/t4gn2z14h |
| Language | English |
| Publisher Date | 1966-05-01 |
| Access Restriction | Open |
| Subject Keyword | Hypersonic Flow Flow Velocity Reentry Vehicle 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 |