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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.
Form Approved REPORT DOCUMENTATION PAGE 0MB No. 0704-0188 Public tel)Ort1ng burden for this collection of information is estimated to average 1 hour per response. induding the time for reviewing instructions, searching exi5ting data sources. gathering and maintain in!,! the data needed, and completing and rev,ew,ng the collection of Information. Send comments r~ardlng tlils burden estimate or any other aspect of this collection of Information, including suggestions tor reducing this burden. tO Washington Headquarters Services, Directorate or Information Operations and Reports, 1215 Jefferwn Davis Highway, Suite 1204, Arlington, VA 12202-4302, and to the Office of Management and Budget. Paperwork Reduction Project(0704-0188), Washington. DC 20503. 1. AGENCY USE ONLY (Leave blank) ~.• REPORT DATE 13. REPORT TYPE AND DATES COVERED . eptember 10, 1996 Final 4. TITLE AND SUBTITLE 5. FUNDING NUMBERS f.1odeling Unlikely Space-Booster Failures in Risk Galculations C: F04703-91-C-o112 TA:10/95-TT 6. AUTHORW • James A. ard, Jr. Robert M. Montgomery 7. PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES) 8. PERFORMING ORGANIZATION REPORT NUMBER Research Triangle Institute * ACTA, Inc. ** RTl/5180m-43F3000 N. Atlantic Avenue · Skypark311 Cocoa Beach, FL 32931 23430 Hawthorne Blvd., Suite 300 Torrance, CA 90505 9. SPONSORING/MONITORING AGENCY NAME(S) AND ADDRESS(ES) 10. SPONSORING/ MONITORING AGENCY REPORT NUMBER Department of the Air Force (AFSPC) Department of the Air Force (AFSPC) 30th Space Wing 45th Space Wing r\~'1~.1 - -m.-t1<a-a-Vandenberg AFB, CA 93437 Patrick AFB, FL 32925 -Mr. Martin Kinna (30 SW/SEY) Louis J. Ullian, Jr. (45 SW/SED) 11. SUPPLEMENTARY NOTES * Subcontractor " Prime Contractor 12a. DISTRIBUTION/AVAILABILITY STATEMENT 12b. DISTRIBUTION CODE Distribution authorized to US Government agencies and their contractors to protect administrative/operational use data; 10 September 96. Other requests for this document shall be referred to the 30th Space Wing (AFSPC) Safety Office (30 SW/SE),Vandenberg AFB, CA 93437, or 45th Space Wing (AFSPC) Safety Office (45 SW/SE), Patrick AFB, FL 32925. (!__, 13. ABSTRACT (Maximum 200 words) Missile and space-vehicle performance histories contain many examples of failures that cause, or have the potential to cause, significant vehicle deviations from the intended flight line. In RTl's risk-analysis program, DAMP, such failures are referred to as Mode-5 failure responses. Although Mode--5 failure responses are much less likely to occur than those that result in impacts near the flight line, risk-analysis studies are incomplete without them. This report shows how Impacts from Mode-6 failures are modeled in program DAMP. The impact density function used for this purpose contains two shaping constants that control the rate at which the density function drops In value as the angular deviation from the flight line and the impact range increase. Certain Mode--5 •malfunctions are simulated, and the two shaping constants then chosen by trial and error so that impacts from the simulated malfunctions and the theoretical density function are in close agreement. An appendix to the report contains alisting and brief narrative failure history of the A~as, Delta, and Titan missile and space-vehicle launches from the Eastern and Western Ranges from the beginning of each program through August 1996. Each entry gives the vehicle configuration, whether the flight was asuccess, the flight phase in which any anomalous behavior occurred, and aclassification of vehicl~ behavior in accordance with defined failure-response modes. 14. SUBJECT TERMS 15. NUMBER OF PAGES· launch risk, unlikely failure modeling, booster failure probabilities 180 16. PRICE CODE 17. SECURITY CLASSIFICATION 18. SECURITY CLASSIFICATION 19. SECURITY CLASSIFICATION 20. LIMITATION OF ABSTRACT OF REPORT OF THIS PAGE OF ABSTRACT Unclassified lJnclassified lnclasslfled SAR NSN 7540-01-280-5500 Standard Form 298 (Rev. 2-89) Prescribed by AIIISI Std. Z39-18 298·102
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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.