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Results of A M = : 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel (IH-42) / / by John Marroquin
| Results of A M = : 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel (IH-42) / / by John Marroquin |
| Autore | Marroquin J. |
| Pubbl/distr/stampa | Houston, Texas : , : Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, , March 1985 |
| Descrizione fisica | 1 online resource (iii, 27 pages) : illustrations |
| Collana | NASA/CR |
| Soggetto topico |
Aerothermodynamics
Hypersonic heat transfer Aerodynamic heat transfer Hypersonic speed Wind tunnel tests |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Results of A M = 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel |
| Record Nr. | UNINA-9910709972703321 |
Marroquin J.
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| Houston, Texas : , : Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, , March 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility (VKF) 40-inch supersonic and the 50-inch hypersonic wind tunnels A & C (IH-97A/B/C) / / J. Marroquin
| Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility (VKF) 40-inch supersonic and the 50-inch hypersonic wind tunnels A & C (IH-97A/B/C) / / J. Marroquin |
| Autore | Marroquin J. |
| Pubbl/distr/stampa | Houston, Texas : , : Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, , March 1985 |
| Descrizione fisica | 1 online resource (iv, 164 pages) : illustrations |
| Collana | NASA/CR |
| Soggetto topico |
Wind tunnel tests
Aerodynamic heating External tanks Space shuttles Mach number |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility |
| Record Nr. | UNINA-9910709972903321 |
|
Marroquin J.
|
||
| Houston, Texas : , : Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, , March 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Results of the AFRSI rewaterproofing systems screening test in the NASA/AMES Research Center (ARC) 2x2-foot transonic wind tunnel (OS-310) / / J. Marroquin and R.B. Kingsland
| Results of the AFRSI rewaterproofing systems screening test in the NASA/AMES Research Center (ARC) 2x2-foot transonic wind tunnel (OS-310) / / J. Marroquin and R.B. Kingsland |
| Autore | Marroquin J. |
| Pubbl/distr/stampa | Houston, Texas : , : Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, , March 1985 |
| Descrizione fisica | 1 online resource (iii, 113 pages) : illustrations |
| Collana | NASA/CR |
| Soggetto topico |
Fluid flow
Failure analysis Wind tunnel tests Flow distribution Subsonic speed |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Results of the AFRSI rewaterproofing systems screening test in the NASA/AMES Research Center |
| Record Nr. | UNINA-9910709972803321 |
|
Marroquin J.
|
||
| Houston, Texas : , : Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, , March 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
