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Graphical techniques to assist in pointing and control studies of orbiting spacecraft / / Leonard Howell and Joseph H. Ruf
| Graphical techniques to assist in pointing and control studies of orbiting spacecraft / / Leonard Howell and Joseph H. Ruf |
| Autore | Howell Leonard W. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , March 1986 |
| Descrizione fisica | 1 online resource (iv, 15 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Hubble Space Telescope
Computer graphics Pointing control systems Orbital mechanics Spacecraft models Space vehicles - Control systems |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709713503321 |
Howell Leonard W.
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , March 1986 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Proposed flight research of a dual-bell rocket nozzle using the NASA F-15 airplane / / Daniel S. Jones and Trong T. Bui, Joseph H. Ruf
| Proposed flight research of a dual-bell rocket nozzle using the NASA F-15 airplane / / Daniel S. Jones and Trong T. Bui, Joseph H. Ruf |
| Autore | Jones Daniel S. |
| Pubbl/distr/stampa | Edwards, CA : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , September 2013 |
| Descrizione fisica | 1 online resource (17 pages) : illustrations (some color) |
| Collana | NASA/TM |
| Soggetto topico |
Altitude tests
F-15 aircraft Flight tests Flow distribution Nozzle design Nozzle geometry |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702416503321 |
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Jones Daniel S.
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| Edwards, CA : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , September 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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