General Characteristics
- Primary Function: Space booster
- Builder: Martin Marietta
- Power Plant:
- Stage 0 consists of two solid rocket motors.
- Stage 1 uses two LR87 liquid propellant engines.
- Stage 2 uses one LR91 liquid propellant engine.
- Stage 3 uses two Aerojet AJ-10-138 liquid propellant engines.
- Length: 42 m
- Stage 0: 25.91 m
- Stage 1: 22.28 m
- Stage 2: 7.9 m
- Stage 3: 4.57 m
- Diameter:
- Stage 0: 3.05 m
- Stage 1: 3.05 m
- Stage 2: 3.05 m
- Stage 3: 3.05 m
- Mass:
- Stage 0: Empty 33,798 kg/ea; Full 226,233 kg/ea
- Stage 1: Empty 5,443 kg; Full 116,573 kg
- Stage 2: Empty 2,653 kg; Full 29,188 kg
- Stage 3: Empty 1,950 kg; Full 12,247 kg
- Lift capability:
- Up to 28,900 lb (13,100 kg) into a low-earth orbit with 28 degrees inclination.
- Up to 6,600 lb (3,000 kg) into a geosynchronous transfer orbit when launched from Cape Canaveral Air Force Station, FL.
- Maximum takeoff weight: 626,190 kg
- Cost:
- Date deployed: June 1965.
- Launch sites: Cape Canaveral Air Force Station, FL., and Vandenberg Air Force Base, CA.
Read more about this topic: Titan IIIC
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