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Titan 3L4
Part of Titan
Titan 3L4
Titan 3L4
Credit: © Mark Wade
American orbital launch vehicle. Variant of Titan with 15 foot Large Diameter Core, 4 x 7 segment strap-ons. Man rated, optimized for delivery of 40,000 pound manned payloads into 250 nm / 50 deg space station orbit.

Status: Study 1965. Payload: 45,000 kg (99,000 lb). Thrust: 25,642.10 kN (5,764,573 lbf). Gross mass: 1,747,580 kg (3,852,750 lb). Height: 63.00 m (206.00 ft). Diameter: 4.57 m (14.99 ft). Apogee: 185 km (114 mi).

LEO Payload: 45,000 kg (99,000 lb) to a 185 km orbit. Payload: 16,000 kg (35,000 lb) to a GTO. Launch Price $: 38.000 million in 1965 dollars.

Stage Data - Titan 3L4



Family: orbital launch vehicle. Country: USA. Engines: LR87-7, LR91-7, RL-10A-3. Stages: Titan LDC-1, Titan LDC-2, Centaur D/E, UA1207. Agency: Martin.

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