Results of investigation conducted in Langley 8-ft transonic pressure tunnel on vehicle designed to use heat sink and blunt shape to alleviate effects of heating encountered during reentry of earth's atmosphere.
Wind-tunnel investigation at mach numbers from 0.40 to 1.14 of static aerodynamic characteristics of nonlifting vehicle suitable for reentry
NASA -- Memo
National Aeronautics and Space Administration -- Memorandums ; Memo n 4-13-59L
1959
14 pages
Report
English
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