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Dow Uap D48 Report September 1996
Page 75
75 / 181
Figure 27 shows the percentages of malfunction-turn impacts in 5° sectors for no
breakup and for breakup qa’s of 20,000, 10,000, and 5,000 deg-Ib/: ft. For B= 1,000,
theoretical Mode-5 impact distributions are also plotted in the figure using best-fit
values of A. This value of B was chosen since it is currently used by RTI in making
launch-area risk studies for 45SW/SE. Within the sectors from +60° to +180°, where
most population centers are located, data fits are reasonably good. As seen in the next
figure, the divergence for the no-breakup case can be greatly reduced by'selecting other
values for B and A.
100
10
Percent in 5-deg sector (%)
0.1
i i i i i i i
0 20 40 60 80 100 120 140 160 180
Angle From Flight Path (deg)
Figure 27. Titan Simulation Results with B = 1,000
9/10/96 66 RII
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