Documents / Report
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.
“Mission Control”17 pages
c. Insertion of improper computer programs d. Support-personnel fatigue A third limitation of the parts-analysis approach discussed in Ref. [4] deals with the subjectivity and invalid assumptions often used to· estimate piece/component reliabilities. Here Booz•Allen quotes from a reporf1 by the Office of Technology Assessment, and we do likewise: "The design reliability of proposed vehicles is generally estimated using: Data from laboratory tests of vehicle systems (e.g., engines and avionics) and components that have already been built; Engineer's judgments about the reliability- achievable in systems and components that have not been built; Analyses of whether a failure in one system or component would cause other systems and components, or the vehicle to fail; and Assumptions (often tacit) that: the laboratory conditions under which systems were tested precisely duplicate the conditions under which the systems will operate, the conditions under which the system will operate are those under which theywere designed to operate, the engineer's judgments about reliability are correct, and the failure analyses considered all circumstances and details that influence reliability: Such engineering estimates of design·reliability are incomplete and subjective...". Effects influencing reliability that the analyst may fail to consider include: a. Lightning strikes b. Aging effects, particularly for solid propellants c. Corrosion d. Insufficient heat or cold insulation for critical components e.Idng f. Erroneous antennae patterns or instrumentation Booz• Allen concludes as follows:· ''Finally, due to its nature, the engineering approach can not account for undetected design flaws. (If these flaws were detected, and could be modeled, 9/10/96 14 RTI
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Report, from the pursue collection. The PDF is mirrored here; the original link is under it. 181 pages are in the text index: search them above, or from the library's search.