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Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight / / Scott R. Thomas, H. Douglas Perkins, and Charles J. Trefny
| Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight / / Scott R. Thomas, H. Douglas Perkins, and Charles J. Trefny |
| Autore | Thomas Scott R. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , March 1997 |
| Descrizione fisica | 1 online resource (10 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Ejectors
Hydrocarbon fuels Wind tunnel tests Supersonic speed Mach number Engine tests Propulsion system performance Flow distribution |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707625903321 |
Thomas Scott R.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , March 1997 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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SRM-assisted trajectory for the GTX reference vehicle / / John Riehl and Charles Trefny, Daniel Kosareo
| SRM-assisted trajectory for the GTX reference vehicle / / John Riehl and Charles Trefny, Daniel Kosareo |
| Autore | Riehl John |
| Pubbl/distr/stampa | Cleveland Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , June 2002 |
| Descrizione fisica | 1 online resource (16 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Solid propellant rocket engines
Launch vehicles Hypersonic combustion Trajectory optimization |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Solid-rocket motors-assisted trajectory for the GTX reference vehicle |
| Record Nr. | UNINA-9910705699803321 |
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Riehl John
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| Cleveland Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , June 2002 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system / / J.R. DeBonis and C.J. Trefny
| Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system / / J.R. DeBonis and C.J. Trefny |
| Autore | DeBonis James R. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , February 2001 |
| Descrizione fisica | 1 online resource (18 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Air breathing boosters
Hypersonic speed Computational fluid dynamics Wind tunnel tests Propulsion Pressure distribution |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Supersonic wind tunnel tests of a half-axisymmetric 12 degree spike inlet to a rocket-based combined-cycle propulsion system |
| Record Nr. | UNINA-9910706590803321 |
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DeBonis James R.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , February 2001 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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