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.