Comparison of Space Shuttle Orbiter Wing Leading Edge Heating Rate Calculations with Experimental and Flight Data
32nd Meeting, Aerospace sciences ; 1994 ; Reno; NV
1994-01-01
ALL
Separate papers nos AIAA 94-0047 - 94-0872 with gaps held only
Conference paper
English
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British Library Conference Proceedings | 1994
|Dynamic Impact Tolerance of Space Shuttle Orbiter Wing Leading-Edge Panels
Online Contents | 2008
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