Department of the Air Force Report, 1996

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100
Atlas HAS Random-Attitude Failures through 280 sec
Breakup q-alpha in deg-lb/ft²
no breakup
20,000
10,000
5,000
10
Percent in 5-deg sector (%)
B = 500,000
A = 4.00
A = 4.80
A = 5.30
A = 5.55
1
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
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RTI