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. 155 D.4 Titan Launch and Performance History The Titan family of launch vehicles was established in…
  • p. 160 …GEMINI GT-4 06/03/65 II (G-4) ER 0 120 GOLD FISH 06/14…
  • p. 161 …30/65 II (B-4) WR 5 2 0 132 SV: GEMINI GT-7 12/04…
Shortly after the Challenger accident in 1986, when the US government decided to
offload commercial payloads from the Space Shuttle, Martin Marietta announced plans
to develop a Titan III commercial launch vehicle with its own funds. The commercial
Titan III is derived from the Titan 34D with a stretched second stage and a bulbous
shroud for dual or dedicated payloads. The first commercial Titan III was launched
with two communications satellites in December 1989. Table 44 shows a summary of
Titan space-vehicle configurations since Gemini.1101
Confi ation
II Gemini
IIIB
34B
IIIC
HID
IIIE
34D
IISLV
III Commercial
IV
9/10/96
Table 44. Summa of Titan Vehicle Confi rations
Descri
Titan II ICBM converted to a man-rated vehicle
Same as Titan II Gemini except stretched stages 1 and 2, and an
inte al Trans
Same as IIIA e
Same as IIIC ex
·Same as 34B with added 5½-segment SRMs. Uses either Transtage
orIUSu e
Refurbished II ICBM with 10-foot diameter PLF
Same as 34D except stretched stage 2, single or dual carrier,
enhanced liquid-rocket engines, and 13.1-foot diameter PLF. Can
use PAM-D2, Transta e, or TOS u er sta e
Same as 34D except stretched stages 1 and 2, 7-segment SRM or 3-
segment SRMU, and 16.7-foot diameter PLF. Can use IUS or
Centaur u er sta e
147 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.