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DOW-UAP-D48, Department of the Air Force Report, 1996
Page 51
51 / 181
In Figure 9, the percentages of impacts in 5 sectors from 0 to 180 have been plotted
for Atlas IIAS random-attitude turns out to 280 seconds. (It should be remembered that
random-attitude turns are representative of combined random-attitude and slow turns.)
For B = 1000, theoretical Mode-5 impact percentages are also plotted in the figure for
best-fit values of A obtained by trial and error.
100
Atlas tAS Random-Attitude Failures through280 sec
Breakup-q-alphain deg-lb/ft
no breakup
20,000
10,000
Percent in 5-deg sector (%)
5,000
10
B1,000
A=1.90
A=2.75
A...3.20.
A = 3.45
0.1
0
20
40
60
80
100
120
140
160
180
Angle From Flight Path (deg).
Figure 9. Atlas IIAS Simulation Results with B = 1,000
By observing curve shapes, it can perhaps be seen that no single value of A causes a
theoretical impact distribution and a distribution of impacts from random-attitude
turns to match closely over the entire range of 5 sectors. Attempts to improve the
match on one end of the curve by selecting a different A merely degrades the match on
9/10/96
42
RTI
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