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Operationally efficient propulsion system study (oepss) data book. volume 10; air augmented rocket afterburning
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Farhangi, Shahram |
| Editor | Trent, Donnie |
| Copyright Year | 1992 |
| Description | A study was directed towards assessing viability and effectiveness of an air augmented ejector/rocket. Successful thrust augmentation could potentially reduce a multi-stage vehicle to a single stage-to-orbit vehicle (SSTO) and, thereby, eliminate the associated ground support facility infrastructure and ground processing required by the eliminated stage. The results of this preliminary study indicate that an air augmented ejector/rocket propulsion system is viable. However, uncertainties resulting from simplified approach and assumptions must be resolved by further investigations. |
| File Size | 1406844 |
| Page Count | 42 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19980041407 |
| Archival Resource Key | ark:/13960/t3518x89n |
| Language | English |
| Publisher Date | 1992-10-30 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Rocket Nozzles Cooling Propulsion System Performance Single Stage To Orbit Vehicles Rocket Engines Advanced Launch System Sts Ground Support Systems Air Flow Drag Ejectors Thrust Augmentation Inviscid Flow Rocket Engine Design Afterburning Boundary Layers Mach Number 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 |
