◆ SpookStack

Figure 31 shows that a good fit for the no-breakup case is possible if higher values of B. and A are used. The simulated malfunction-turn impact distributions for the breakup. cases plotted in this figure are identical with those in Figure 30. Since the theoretical percentages for B = 1,000 produced excellent fits, these values were simply replotted in Figure 31. For the no-breakup case, various combinations of B and A were tried before arriving at the plot shown in the figure. 100 LLV1Random-AttitudeFaituresthrough290 sec Breakup q-alphain-deg-lb/ft no breakup 20,000 10,000 10 Percent in 5-deg sector (%) 5,000 A245B10,000 A=2.60B1000 A=270B1,000 A = 2.75, b 1,000 0.1 0.01 0 20 40 60 80 100 120 140 160 180 Angle From Flight Path (deg) Figure 31. LLV1 Simulation Results with Best-Fit Shaping Constants. 9/10/96 71 RTI