Titan 2B (original) (raw)

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Titan 2B

Part of Titan

American intercontinental ballistic orbital launch vehicle. Space launch version of Titan 2 ICBM, obtained through minimal modification of ICBM (new wiring and avionics only, and use of existing ICBM re-entry vehicle shroud). Proposed in the late 1980's but never developed.

Payload: 3,175 kg (6,999 lb). Thrust: 2,090.00 kN (469,850 lbf). Gross mass: 154,000 kg (339,000 lb). Height: 31.40 m (103.00 ft). Diameter: 3.05 m (10.00 ft). Apogee: 185 km (114 mi).

LEO Payload: 3,175 kg (6,999 lb) to a 185 km orbit at 28.60 degrees.

Family: ICBM, orbital launch vehicle. Country: USA. Stages: Titan 2-1, Titan 2-2. Agency: Martin.

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