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Composite engines for application to a single-stage-to-orbit vehicle
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Piercy, T. G. Bendot, J. G. Brown, P. N. |
| Copyright Year | 1975 |
| Description | Seven composite engines were designed for application to a reusable single-stage-to-orbit vehicle. The engine designs were variations of the supercharged ejector ramjet engine. The resulting performance, weight, and drawings of each engine form a data base for establishing a potential of this class of composite engine to various missions, including the single-stage-to-orbit application. The impact of advanced technology in the design of the critical fan turbine was established. |
| File Size | 3005522 |
| Page Count | 101 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760006115 |
| Archival Resource Key | ark:/13960/t1dk06q9w |
| Language | English |
| Publisher Date | 1975-12-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Turboramjet Engines Tables Data Equipment Specifications Performance Tests Structural Weight Gas Generators Engine Design Engine Tests Reusable Launch Vehicles Computer Programs 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 |
