John Company

Department of the Air Force Report, 1996

DOW-UAP-D048 · page 48 of 181

Page 48 of 181 of DOW-UAP-D048

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9/10/96
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Atlas IIAS Impacts
Random-Attitude Failures at 130 sec.
Thrust to 280 sec.
No Breakup
39
Figure 7. Atlas IIAS Impacts with No Breakup
RTI