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 9/10/96 Vl RTI
Vision Description (EN)
A single page of a technical report, numbered '2' at the bottom. The text discusses 'Mode-5 failure-response methodology' and 'impact-density functions' related to flight safety for vehicles like Atlas, Delta, and Titan. The page contains no redactions; all text is fully legible, including a date of 9/10/96 and the acronym RTI.
Descrição Vision (PT-BR)
Uma única página de um relatório técnico, numerada como '2' na parte inferior. O texto discute a 'Mode-5 failure-response methodology' e 'impact-density functions' relacionadas à segurança de voo para veículos como Atlas, Delta e Titan. A página não contém rasuras (redactions); todo o texto está totalmente legível, incluindo a data 9/10/96 e a sigla RTI.