Loading...
Please wait, while we are loading the content...
Similar Documents
Airframe-integrated propulsion system for hypersonic cruise vehicles
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Jones, R. A. Huber, P. W. |
| Copyright Year | 1978 |
| Description | Research on a new, hydrogen burning, airbreathing engine concept which offers good potential for efficient hypersonic cruise vehicles is considered. Features of the engine which lead to good performance include; extensive engine-airframe integration, fixed geometry, low cooling, and the control of heat release in the supersonic combustor by mixed-modes of fuel injection from the combustor entrance. The engine concept is described along with results from inlet tests, direct-connect combustor tests, and tests of two subscale boiler-plate research engines presently underway at conditions which simulate flight at Mach 4 and 7. |
| File Size | 658975 |
| Page Count | 7 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19790013253 |
| Archival Resource Key | ark:/13960/t09w57t22 |
| Language | English |
| Publisher Date | 1978-01-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Structural Design Propulsion System Performance Engine Design Airframes Supersonic Combustion Ramjet Engines Cooling Systems Fuel Injection Propulsion System Configurations Aircraft Configurations Hypersonic Vehicles Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
