Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber / / Mary F. Wadel
| Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber / / Mary F. Wadel |
| Autore | Wadel Mary F. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , June 1997 |
| Descrizione fisica | 1 online resource (11 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Combustion chambers
High aspect ratio Cooling Channels Computer programs Design |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910708661203321 |
Wadel Mary F.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , June 1997 | ||
| Lo trovi qui: Univ. Federico II | ||
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Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber with development of an optimized design / / by Mary F. Wadel
| Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber with development of an optimized design / / by Mary F. Wadel |
| Autore | Wadel Mary F. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , January 1998 |
| Descrizione fisica | 1 online resource (approximately 78 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Rocket engines
Aspect ratio Combustion chambers |
| Soggetto genere / forma | Academic theses. |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717122203321 |
Wadel Mary F.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , January 1998 | ||
| Lo trovi qui: Univ. Federico II | ||
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Validation of high aspect ratio cooling in a 89 kN (20,000 lbf) thrust combustion chamber / / Mary F. Wadel and Michael L. Meyer
| Validation of high aspect ratio cooling in a 89 kN (20,000 lbf) thrust combustion chamber / / Mary F. Wadel and Michael L. Meyer |
| Autore | Wadel Mary F. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , June 1996 |
| Descrizione fisica | 1 online resource (10 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Rocket engines
Combustion chambers Thrust chambers Mass flow Liquid hydrogen Cooling High aspect ratio Performance tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Validation of high aspect ratio cooling in a 89 kN |
| Record Nr. | UNINA-9910707356003321 |
Wadel Mary F.
|
||
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , June 1996 | ||
| Lo trovi qui: Univ. Federico II | ||
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