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Department of the Air Force Report, 1996

U.S. Department of War · 1996-09-10 · 181 pages · text from the file's own layer

This final report, dated September 10, 1996, was prepared by the Research Triangle Institute for the Department of the Air Force's 45th and 30th Space Wing safety offices. Titled Modeling Unlikely Space-Booster Failures in Risk Calculations, it shows how rare Mode-5 failures, in which a rocket veers well off its intended flight line, are modeled in the DAMP risk-analysis program. An appendix lists Atlas, Delta, Titan and Thor launch and failure histories through August 1996.

From the source:Release of 2026-05-08 Incident: 9/10/96, N/A. This report describes the Modeling of Unlikely Space-Booster Failures in Risk Calculations, documenting historical launch failure modes and recommending corrective actions to address them using novel modelling techniques.

  • p. 5 …64 6.4 Shaping Constants for Titan IV................................................................................ 65 6.5 Shaping Constants for LLVl .................................................................................... 69…
  • p. 74 …6.4 Shaping Constants for Titan IV Mode-5 shaping constants for Titan IV were developed…
  • p. 77 …Shaping Constants for Titan IV TB (sec) Breakupqa (deg-lb/ft2) B A II 300 none…
  • p. 109 …Titan IIIC and later configurations to include IIIB, IIID, IIIE, 34B, 34D, III/CT, IV, II…
  • p. 155 …Titan II SLV was developed from refurbished Titan II ICBMs incorporating technology and hardware from the…
  • p. 156 …Summa of Titan Vehicle Confi rations Descri Titan II ICBM converted to a man-rated vehicle…
  • p. 159 …2 0 54 WS (first Titan II) 03/16/62 II (N-2) ER 0 55…
  • p. 160 …08/13/64 II (8-7) WR 0 104 SV (first Titan Ill) 09/01/64…
  • p. 166 D.4.2 Titan Failure Narratives The following narratives provide available details about each Titan failure…
  • p. 168 …Stage II engine shut down prematurely due to oxidizer bootstrap-line failure. 76. Titan I (Mares…
  • p. 169 …Titan II (Thread Needle), 20 June 63, Response Mode 5, Flight Phase 2: Flight appeared normal…
  • p. 170 …Titan II (Bold Guy), 21 Sep 65, Response Mode 4, Flight Phase 2: After a normal…
  • p. 172 …Following a successful Titan-II second-stage burn and after payload separation, the apogee- kick motor…
F = 0.8, only the most recent 25 or so data points contribute to the final result, since all
older data points are essentially weighted out of the solution.
1.0
0.9
0.8
0.7
...-i:!: 0.6
u..
-.c- 0.5 ........ ............ i ..........................J ...........................+········--
F = ~ (equally weighted)
! F=0.J9 I
! I--.: ···········;···························
....--········-----···--
···· -•-1- +-=0.9! 5 !
C)
·a5 i I~ ' ............................ ~............................
ca 0.4
Cl
0.3
0.2
0.1
0.0
ca
i --
0.99
..... ...........................:.......
. ..... 1 /.-····---;
-----i·········· -1..................
+o.s .......... ,
I
0 50 100 150 200 250 300
Data Index (older->)
Figure 35. Exponential Weights for Fading-Memory Filters
For the exponentially-weighted fading-memory filter, it can be shown that the
recursive filter factor used in Eq. (12) is
1-F
a=-- (20)
n 1-Fn
Since OS F S 1, an in Eq. (20) does not approach zero as n approaches infinity (as the
other two filters do), but instead approaches the value (1 - F). If F = 0, then an= 1 for all
n, the filter has no memory at all, and the filtered value always equals the last
measurement. In the limit as F approaches one, L'Hospital' s rule can be applied to
9/10/96 93 RTI

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Report, from the pursue collection. The PDF is mirrored here; the original link is above. 181 pages are in the text index: search them above, or from the library's search.