Editing Titan IIIC (section)

==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 rocket propellants|liquid propellant]] engines.
**Stage 2 uses one LR91 [[Liquid rocket propellants|liquid propellant]] engine.
**Stage 3 uses two Aerojet [[AJ-10| AJ-10-138]] [[Liquid rocket propellants|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&nbsp;kg/ea; Full 226,233&nbsp;kg/ea
**Stage 1: Empty 5,443&nbsp;kg; Full 116,573&nbsp;kg
**Stage 2: Empty 2,653&nbsp;kg; Full 29,188&nbsp;kg
**Stage 3: Empty 1,950&nbsp;kg; Full 12,247&nbsp;kg
*Lift capability:
**Up to 28,900&nbsp;lb (13,100&nbsp;kg) into a low Earth orbit with 28 degrees inclination.
**Up to 6,600&nbsp;lb (3,000&nbsp;kg) into a geosynchronous transfer orbit when launched from [[Cape Canaveral Air Force Station]], FL.
*Maximum takeoff weight:  626,190&nbsp;kg
*Cost:
*Date deployed: June 1965.
*Launch sites: [[Cape Canaveral Air Force Station]], FL., and [[Vandenberg Air Force Base]], CA.