Titan 2S

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Titan 2S

Part of Titan

American intercontinental ballistic orbital launch vehicle. Version of refurbished Titan 2 ICBM with two to eight Castor 4A solid-propellant strap-on stages. Proposed in the late 1980's but never developed.

Payload: 9,000 kg (19,800 lb). Gross mass: 247,000 kg (544,000 lb). Height: 35.00 m (114.00 ft). Diameter: 3.05 m (10.00 ft). Span: 9.60 m (31.40 ft). Apogee: 185 km (114 mi).

Larger GEM-40 motors were also proposed. Would have required development of a new skirt for the first stage for attachment of the solid boosters.

LEO Payload: 9,000 kg (19,800 lb) to a 185 km orbit at 28.60 degrees.

Family: ICBM, orbital launch vehicle. Country: USA. Agency: Martin.

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