John Company

Department of the Air Force Report, 1996

DOW-UAP-D048 · page 9 of 181

Page 9 of 181 of DOW-UAP-D048

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Table 19. Sample Impact Distribution for Atlas IIAS-with No Breakup .......................... 41
Table 20. Shaping Constants for Atlas IIAS......................................................................... 48
Table 21. Shaping Constants and Related Risks for Atlas HAS­......................................... 50
Table 22. Best-Fit Conditions for Atlas IIAS............................................. : .......................... 52
Table 23. Shaping Constants and Related Risks for Delta-GEM ....................................... 64
Table 24. Shaping Consta.nts for Titan IV ............................................................................ 68
Table 25. Shaping Constants for LLVl ................................................................................. 72
Table 26. Summary of A Values for B = 1,000................. ; ................................................... 72­
Table 27. Failure Probabilities for Atlas, Delta, and Titan ................................................. 75
Table 28. Recommended Response-Mode Percentages for Flight Phases O-2 ................. 75~
Table 29. Recommended Response-Mode Percentages for Flight Phases O - 1................ 75
Table 30. Absolute Failure Probabilities for Response Modes 1 - 5 .................................. 76
Table 31. Summary of A Values for B = 1,000.................................................................. • ... 77
Table 32. Summary of Optimum·Mode-5 Shaping Constants ........................................... 77
Table 33. Effect on £-Ratio-of Varying Mode-5 Constant A {B = 1000) - Part 1 ................ 82
Table 34. Effect on £-Ratio-of Varying Mode-5 Constant A {B = 1000) - Part 2 ................ 83
Table 35. Effect on £-Ratio-of Varying Mode-5 Constant B {A = 3) - Part 1 ...................... 84
Table 36. Effect on £-Ratio-of Varying Mode-5 Constant B {A= 3) - Part 2 ...................... 85
Table 37. Filter Application for Failure Probability ............................................................ 95
Table 38. Flight-Phase Defi°:,itions........................................................................................ 99
Table 39. Flight Phases by Launch Vehicle ......................................................................... 99
Table 40. Summary of Atlas Vehicle Configurations ....................................................... 101
Table 41. Atlas Launch History ........................................................... • ............................... 103
•Table 42. Summary of Delta Vehicle Configurations ....................................................... 133
Table 43. Delta Launch History .......................................................................................... 136
Table 44. Summary of Titan Vehicle Configurations ....................................................... 147 .
Table 45. Titan Launch History .......................................................................................... 149
Table 46. Thor Launch History ........................................................................................... 165
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