Department of the Air Force Report, 1996
DOW-UAP-D048 · page 77 of 181
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The best-fit values of B and A shown in Figure 27 and Figure 28 are tabulated for convenient reference in-Table 24. For breakup qa's of 10,000 and 5,000 deg-lb/ft2, the currently-used value of B = 1,000 provided a better data fit than other values of B that were investigated. Table 24. Shaping Constants for Titan IV TB (sec) Breakupqa (deg-lb/ft2) B A II 300 none 20,000 10,000 5,000 1,000 2.00 2.95 3.25 3.50 300 none 20,000 10,000 5,000 10,000 2,000 1,000 1,000 2.70 3.15 3.25 3.50 Risk calculations in the launch area were not made for Titan IV. 9/10/96 68 RTI