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Fairing separation analysis using SepTOOL / / Bart F. Zalewski and William B. Dial, Daniel N. Kosareo
| Fairing separation analysis using SepTOOL / / Bart F. Zalewski and William B. Dial, Daniel N. Kosareo |
| Autore | Zalewski Bartlomiej Francisze |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2015 |
| Descrizione fisica | 1 online resource (18 pages) : color illustrations |
| Collana | NASA/CR |
| Soggetto topico |
Spreadsheets
Computer programs Launch vehicles Launch vehicle configurations Spacecraft trajectories |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910703877403321 |
Zalewski Bartlomiej Francisze
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2015 | ||
| 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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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 |
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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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