Info
- Utilizzare la checkbox di selezione a fianco di ciascun documento per attivare le funzionalità di stampa, invio email, download nei formati disponibili del (i) record.
Entry, descent, and landing with propulsive deceleration : supersonic retropropulsion wind tunnel testing / / Bryan Palaszewski
| Entry, descent, and landing with propulsive deceleration : supersonic retropropulsion wind tunnel testing / / Bryan Palaszewski |
| Autore | Palaszewski Bryan Alan Richard |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
| Descrizione fisica | 1 online resource (25 pages) : illustrations |
| Collana | NASA/TM 2012-217746 |
| Soggetto topico |
Computational fluid dynamics
Planetary landing Aerodynamic brakes Landing aids Soft landing Landing sites Rocket engines Shock wave interaction Supersonic flight |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Entry, descent, and landing with propulsive deceleration |
| Record Nr. | UNINA-9910704623303321 |
Palaszewski Bryan Alan Richard
|
||
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Max Launch Abort System (MLAS) Landing Parachute Demonstrator (LPD) drop test [[electronic resource] /] / Christopher M. Shreves
| Max Launch Abort System (MLAS) Landing Parachute Demonstrator (LPD) drop test [[electronic resource] /] / Christopher M. Shreves |
| Autore | Shreves Christopher M |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011] |
| Descrizione fisica | 1 online resource (v, 28 pages) : color illustrations, color maps |
| Collana | NASA/TM |
| Soggetto topico |
Drop tests
Parachutes Abort apparatus Soft landing Spacecraft modules Simulators H-53 helicopter |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Max Launch Abort System |
| Record Nr. | UNINA-9910701057803321 |
|
Shreves Christopher M
|
||
| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Payload performance analysis for a reusable two-stage-to-orbit vehicle / / Paul V. Tartabini [and three others]
| Payload performance analysis for a reusable two-stage-to-orbit vehicle / / Paul V. Tartabini [and three others] |
| Autore | Tartabini Paul V. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 2015 |
| Descrizione fisica | 1 online resource (iv, 30 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Reusable launch vehicles
Multistage rocket vehicles Soft landing Reentry effects Spacecraft modules |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Payload performance analysis for a reusable two stage to orbit vehicle |
| Record Nr. | UNINA-9910703878403321 |
|
Tartabini Paul V.
|
||
| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
