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dow-uap-d48-report-september-1996
p009 / 146
 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.