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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.

Table 11. Number of Failures for All Vehicles (1186 Flights)
Flight
Phase 1
Fail
2
ure-Res
3
oonse Mode
4 5 'NA'
3&4
Tumble
0
0-1
0-2
0-3
0-4
0-5
0
13
13
13
13
13
0
4
4
4
4
4
0
3-
3
3
3
3
3
68
129
161
165
165
0
15
27
28
28
28
0
11
29
38
45
53
1
19
33
40
42
42
Table 12. Date of Most Recent Failure
Response Vehicle
Mode Atlas Delta Titan Thor*
1 03/02/65 none 12/12/59 04/19/58
2 12/18/81 none 05/01/63 12/30/58
3 .04/25/61 none none 07/21/59
4 08/22/92 05/03/86 10/05/93 03/24//64
5 12/08/80 08/27/69 11/30/65 01/24/62
*Last Thor launch was 02/23/65
For the reasons advanced previously, an exponential filter has been used to estimate
relative probabilities of occurrence for Modes 1 through 5 and the fraction of Mode-3
and Mode-4 failures that tumble while the vehicle is thrusting. The percentage
weightings for various data samples are shown in Table 13 for values of F from 0.980 to
0.999. Because of the large size of the composite sample (1186), the filter-control
constant of 0.98 used previously to estimate absolute failure probabilities for individual
vehicles does not seem suitable for estimating relative probabilities for the individual
response modes. Use of 0.98 would effectively place 98.2% of the total weight on the
most recent 200 tests thus, in effect, eliminating the earliest 986 tests from the solution.
These are the very tests needed to provide an adequate sample of failures from which
to estimate relative frequencies of occurrence of the individual response modes.
9/10/96 26 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.