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DOW-UAP-D48, Department of the Air Force Report, 1996
Page 55
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100
Atlas ltAS Random-Attitude Failures through 280 sec
Breakup.q-alpha.in-deg-lb/ft
no breakup
20,000
10,000
5,000
Percent in 5-deg sector (%)
10
3=500,000
A4.00
A4.80
A5.30
A..5.55
0.1
0
20
40
60
80
100
120
140
160
180
Angle From Flight Path (deg).
Figure 12. Atlas IIAS Simulation Results with B = 500,000
9/10/96
46
RTI
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