John Company

Department of the Air Force Report, 1996

DOW-UAP-D048 · page 45 of 181

Page 45 of 181 of DOW-UAP-D048

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100
Atlas HAS Failures through 280 sec
Breakup q-alpha = 20,000 deg-lb/ft 2
Random-attitude turns
Stow turns
Combined turns (0.75 random + 0.25 slow)
10
Percent in 5-deg sector (%)
1
0.1
0
20
40
60
80
100
120
140
160
180
Angle From Flight Path (deg)
Figure 5. Combined Random-Attitude and Slow-Turn Results
9/10/96
36
RTI