X-38 experimental aeroheating at Mach 10
Details are provided of a recent effort at the NASA Langley Research Center to extend the experimental aeroheating database for the X-38 program to higher-Mach-number conditions. Global surface heat-transfer distributions were measured on 0.0177- and 0.0236-scale models of the proposed X-38 Rev 8.3...
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Veröffentlicht in: | Journal of spacecraft and rockets 2004-03, Vol.41 (2), p.193-301 |
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Hauptverfasser: | , , , , |
Format: | Artikel |
Sprache: | eng |
Online-Zugang: | Volltext |
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