Entry, descent, and landing with propulsive deceleration : supersonic retropropulsion wind tunnel testing / / Bryan Palaszewski
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| Autore: |
Palaszewski Bryan Alan Richard
|
| Titolo: |
Entry, descent, and landing with propulsive deceleration : supersonic retropropulsion wind tunnel testing / / Bryan Palaszewski
|
| Pubblicazione: | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
| Descrizione fisica: | 1 online resource (25 pages) : illustrations |
| Soggetto topico: | Computational fluid dynamics |
| Planetary landing | |
| Aerodynamic brakes | |
| Landing aids | |
| Soft landing | |
| Landing sites | |
| Rocket engines | |
| Shock wave interaction | |
| Supersonic flight | |
| Note generali: | Title from title screen (viewed Aug. 29, 2013). |
| "December 2012." | |
| "Prepared for the 50th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Nashville, Tennessee, January 9-12, 2012.." | |
| "AIAA-2012-401." | |
| Nota di bibliografia: | Includes bibliographical references (pages 4-6). |
| Altri titoli varianti: | Entry, descent, and landing with propulsive deceleration |
| Titolo autorizzato: | Entry, descent, and landing with propulsive deceleration |
| Formato: | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione: | Inglese |
| Record Nr.: | 9910704623303321 |
| Lo trovi qui: | Univ. Federico II |
| Opac: | Controlla la disponibilità qui |