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Hypersonic cruise aircraft propulsion integration study, volume 2
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Brewer, G. D. Morris, R. E. |
| Copyright Year | 1979 |
| Description | Conceptual vehicle configuration and propulsion approach for a Mach 6 transport aircraft capable of carring 200 passengers 9260 km was investigated. Wind tunnel test data for various hypersonic transport configurations were examined. Canidates for baseline reference vehicles were selected. An explanation of technical methods which were used and configuration details which were significant in the final vehicle concept are given. |
| File Size | 5886281 |
| Page Count | 241 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800006816 |
| Archival Resource Key | ark:/13960/t8z941x2s |
| Language | English |
| Publisher Date | 1979-09-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Aerodynamic Drag Nozzle Geometry Wind Tunnel Tests Aerodynamic Coefficients Aircraft Configurations Propulsion System Configurations Hypersonic Vehicles Yaw 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 |