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Effective thermal conductivities of four metal-ceramic composite coatings in hydrogen-oxygen rocket firings / / by Ralph L. Schacht, Harold G. Price, Jr., and Richard J. Quentmeyer
| Effective thermal conductivities of four metal-ceramic composite coatings in hydrogen-oxygen rocket firings / / by Ralph L. Schacht, Harold G. Price, Jr., and Richard J. Quentmeyer |
| Autore | Schacht Ralph L. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , November 1972 |
| Descrizione fisica | 1 online resource (41 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Rocket firing
Aeronautics Coatings - Thermal properties - Testing Heat - Transmission Composite materials - Effect of temperature on - Testing Rockets (Aeronautics) - Nozzles |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716019603321 |
Schacht Ralph L.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , November 1972 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Two dimensional inviscid jet flow from two nozzles at an angle to a plane surface / / by Marvin E. Goldstein and Robert Siegel
| Two dimensional inviscid jet flow from two nozzles at an angle to a plane surface / / by Marvin E. Goldstein and Robert Siegel |
| Autore | Goldstein Marvin E. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , February 1969 |
| Descrizione fisica | 1 online resource (ii, 42 pages) : illustrations |
| Collana | NASA technical note |
| Soggetto topico |
Jets - Fluid dynamics
Nozzles - Fluid dynamics Rockets (Aeronautics) - Nozzles |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910714093303321 |
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Goldstein Marvin E.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , February 1969 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
