Department of the Air Force Report, 1996

Text

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The simulated impact distributions plotted in Figure 28 are identical to those shown in
Figure 27.
The theoretical Mode-5 percentages were obtained by testing various
combinations of B and A until a good fit between the simulated malfunction-turn
results and theoretical impact-distribution data was obtained in the sectors from ±60° to
±180°. Although somewhat better fits may be possible for the lower breakup qa's, the
effort to find them did not seem worthwhile, since the A's and B's shown in the figure
produced fits that were more than adequate in the sectors where the population centers
are located.
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0
20
40
60
80
100
120
140
160
180
Angle From Flight Path (deg)
Figure 28. Titan Simulation Results with Best-Fit Shaping Constants
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