Titan 23C

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Titan 23C

Part of Titan

American orbital launch vehicle. Post-MOL standardization of Titan 3C, with man-rated systems removed, upgraded first stage engines, digital avionics, blowdown solid rocket motor thrust vector control in place of pressure-regulated system, simplified Transtage attitude control system.

AKA: SLV-5C. Status: Out of production. Payload: 13,100 kg (28,800 lb). Thrust: 10,586.80 kN (2,380,007 lbf). Gross mass: 626,190 kg (1,380,510 lb). Height: 42.00 m (137.00 ft). Diameter: 3.05 m (10.00 ft). Apogee: 185 km (114 mi).

LEO Payload: 13,100 kg (28,800 lb) to a 185 km orbit. Payload: 3,000 kg (6,600 lb) to a GTO.

Family: orbital launch vehicle. Country: USA. Stages: Titan 3A-1, Titan 3A-2, Titan Transtage, UA1205. Agency: Martin.

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