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 Table 44. Summa of Titan Vehicle Confi rations Confi ation Descri II Gemini 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 IIIB 34B Same as IIIA e IIIC HID Same as IIIC ex IIIE 34D ·Same as 34B with added 5½-segment SRMs. Uses either Transtage orIUSu e IISLV Refurbished II ICBM with 10-foot diameter PLF III Commercial 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 IV 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 9/10/96 147 RTI
Vision Description (EN)
This page contains a technical summary of Titan launch vehicle configurations. It includes a paragraph of introductory text followed by 'Table 44. Summary of Titan Vehicle Configurations', which lists various models from II Gemini to IV with brief descriptions of their features. There are no redactions or obscured text on this page.
Descrição Vision (PT-BR)
Esta página contém um resumo técnico das configurações do veículo de lançamento Titan. Inclui um parágrafo de texto introdutório seguido pela 'Table 44. Summary of Titan Vehicle Configurations', que lista vários modelos, de II Gemini a IV, com breves descrições de suas características. Não há rasuras ou texto obscurecido nesta página.