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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…
for example, the risks are over 20 times as great if the vehicle's breakup qa is 20,000
rather than 5,000 deg-lb/ft2.
6.4 Shaping Constants for Titan IV
Mode-5 shaping constants for Titan IV were developed as described in Section 6.3 for
Delta, except that a total of 290,000 simulations were run between the programming
time of 18 seconds and staging at 300 seconds. The percentage of vehicles that break up
during simulated random-attitude turns are plotted against failure time in Figure 26.
The same qa's used with Atlas and Delta were used here, and similar breakup results
were obtained.
100
90
80
-~ 700
........
C:-Q) 60
e
a..
(l) 50
a.::::,
~ 40
Ill
m 30
20
10
0
~ - -...•••••'.•..•••••••••••.... ;•••••••••n•u••••!..•..••••••.....•i••••..••..•••••••••;••.... •••••.. nHHf ■••••
,,,, L,---... 'i i ! Titan IV i i
I ;, ', f' i i i i i
, t1 \: \ r ! r 1 2 r
I : i \ i <ii-alpha iin deg-lb/ft i
... ·t,·t·····! :~....i... ·····+·····.............!····..............+.................+..................f.....I : : \ \ : : : : :
1 / i i \ , I + q-alpha = ~,000 i
•• ,1·/······i r·1···,··· ···t·········....::.-:i:··:::··c:Falpn·a·;;;·tn;ooo-···f......
I : : \ , : , : :
l f .......L..........,.,...!..... ~ '1·· ...............--r--g-alpha.=.~loo □....l......
,: ! i '~ i i i i
,: ! \ i ! i !
■ n••••••• ■ nn 1••••••••••.. •••••••~••nn+ ■ ••••••H ■■ !•••••nnH•••••••j••••••••••••••....t•••••• • •
0 40 80 120 160 200 240 280
Failure Time (sec)
Figure 26. Titan IV Breakup Percentages
9/10/96 65 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.