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Structural sizing of a 25 000-lb payload, air-breathing launch vehicle for single-state-to-orbit / / Joseph M. Roche and Daniel N. Kosareo
| Structural sizing of a 25 000-lb payload, air-breathing launch vehicle for single-state-to-orbit / / Joseph M. Roche and Daniel N. Kosareo |
| Autore | Roche Joseph M. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , January 2001 |
| Descrizione fisica | 1 online resource (10 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Air breathing boosters
Reusable launch vehicles Propulsion system configurations Space transportation |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti |
Structural sizing of a 25,000-lb payload, air-breathing launch vehicle for single-state-to-orbit
Structural sizing of a twenty-five thousand pound payload, air-breathing launch vehicle for single-state-to-orbit |
| Record Nr. | UNINA-9910706579503321 |
Roche Joseph M.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , January 2001 | ||
| 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 |
|
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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