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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…
References
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Launch-Vehicle Debris", RTI/4666/02F, September 19, 1990.
2. Eastern Test Range Directorate of Safety Post-Test Report, Test Dl000, 18 June 1991.
3. Ward, James A., "Baseline Launch-Area Risks for Atlas and Delta Launches",
RTI/5180/60/40F, September 30, 1995.
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Analysis", Draft, Booz•Allen & Hamilton, Inc., 19 February 1992, prepared for the
Air Force Space Command Launch Services Office.
5. "Launch Options for the Future: Special Report", Office of Technology Assessment,
July 1988.
6. Silke, Kevin, 11Reliability Growth Model Overview", General Dynamics Reliability
Bulletin 92-02.
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History Office.
8. "Eastern Range Launches, Chronological Summary", 45th Space Wing History
Office, Extension updating the launch summary through 30 December 1995.
9. "Vandenberg AFB Launch Summary'', Headquarters 30th Space Wing, Office of
History, Launch Chronology, 1958 - 1995.
10. Isakowitz, Steven J., (updated by Jeff Samella), International Reference Guide to Space
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11. Smith, O. G., "Launch Systems for Manned Spacecraft'', Draft, July 23, 1991.
12. "Comparison of Orbit Parameters - Table l", prepared by McDonnell Douglas
Space Systems Company, Delta launches through 4 Nov 95.
13. Missiles/Space Vehicle Files, 45th Space Wing, Wing Safety, Mission Flight Control
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14. Missile Launch Operations Logs, 30th Space Wing, copies provided via ACT A, Inc.,
(Mr. James Baeker), 1963 through 1995.
9/10/96 171 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.