Documents / Report

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…
Launch Vehicle Test Response Flight Rep.
No. Mission/ID Date Confiauratlon Ranae Mode Phase Conf.
307 AFSC 04/18/86 34D-9 WR 4 0 1
308 AFSC 02/11/87 1118/AGENA D {348-11) WR 1
309 AFSC 10/26/87 340-15 WR 1
310 SV-00D 11/29/87 34D-8/Trans. ER 1
311 SV-D00 09/02/88 34D-3/Trans. ER NA 5 1
312 AFSC 09/05/88 11/SLV (23G-1) WR 1
313 AFSC 11/06/88 340-14 WR 1
314 SV-000 05/10/89 340-16/frans. ER 1
315 SV (first T-IV) 06/14189 IV-1/IUS ER NA 1 1
316 SV-DOD 09/04/89 340-2/Trans. ER 1
317 AFSC 09/05/89 11/SLV (23G-2) WR 1
318 SV-JAPAN/UK 01/01/90 Ill ER 1
319 SV-INTELSAT VI 03/14/90 Ill ER NA 2.5&5 1
320 SV-D00 06/08/90 IV-4 ER 1
321 SV-INTELSAT VI 06/23/90 Ill ER 1
322 SV-000 11/13/90 IV-6/IUS ER 1
323 AFSC 03/08/91 IV WR 1
324 AFSC 11/17/91 IV WR 1
325 AFSC 04/25/92 ll/SLV WR 1
326 SV-MARS OBS. · 09/25/92 Ill ER 1
327 AFMC 11/28/92 IV WR 1
328 AFMC 08/02/93 IV (K-11) WR 4 0 1
329 LANDSAT6 10/05/93 11/SLV WR 4 2 1
330 CLEMENTINE 01/25/94 11/SLV WR 1
331 SV-MILSTAR 02/07/94 TIV-CENTAUR (K·10) ER 1
332 SV-D00 05/03/94 TIV-CENTAUR (K-7) ER 1
333 SV-DOD 08/27/94 TIV-CENTAUR {K-9) ER 1
334 SV-D00 12122194 IV-IUS (K-14) ER 1
335 SV-D00 05/14/95 TIV-CENTAUR (K-23) ER 1
336 SV-D00 07/10/95 TIV-CENTAUR (K-19) ER 1
337 SV-MILSTAR 11/06/95 TIV-CENTAUR (K-21) ER 1
338 DOD 04/24/96 TIV-CENTAUR (K-16) ER 1
339 DOD 07/02/96 TIV-NUS (K2) ER 1
9/10/% 156 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.