Department of the Air Force Report, 1996
DOW-UAP-D048 · page 49 of 181
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9/10/96 [ 1 Atlas IIAS Impacts Random-Attitude Failures at 130 sec. Thrust to 280 sec, Breakup q-alpha = 5,000 deg-lb/ft2 40 Figure 8. Atlas IIAS Impacts with Breakup RTI