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The influential aspects of atmospheric disturbances on space vehicle design using statistical approaches for analysis / / by Robert S. Ryan and Alberta W. King
| The influential aspects of atmospheric disturbances on space vehicle design using statistical approaches for analysis / / by Robert S. Ryan and Alberta W. King |
| Autore | Ryan Robert S (Robert Samuel), <1925-> |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , January 1969 |
| Descrizione fisica | 1 online resource (viii, 112 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Aerospace vehicles
Launch vehicles Flight control Atmospheric circulation Launch vehicles (Astronautics) - Design and construction Winds |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716080003321 |
Ryan Robert S (Robert Samuel), <1925->
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| Washington, D.C. : , : National Aeronautics and Space Administration, , January 1969 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Practices in adequate structural design / / Robert S. Ryan
| Practices in adequate structural design / / Robert S. Ryan |
| Autore | Ryan Robert S (Robert Samuel), <1925-> |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Division, , January 1989 |
| Descrizione fisica | 1 online resource (vi, 91 pages) : illustrations |
| Collana | NASA technical paper |
| Soggetto topico |
Flight safety
Management methods Project management Requirements Space shuttles Stress analysis Structural design |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910693061603321 |
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Ryan Robert S (Robert Samuel), <1925->
|
||
| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Division, , January 1989 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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