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Family: Titan. Country: USA. Status: Study 1965.
Variant of Titan with 15 foot Large Diameter Core, 2 x 7 segment strap-ons. Man-rated, optimized for delivery of heavy payloads into LEO. Never developed.
SpecificationsLEO Payload: 35,000 kg. to: 185 km Orbit. Payload: 12,000 kg. to a: Geosynchronous transfer trajectory. Liftoff Thrust: 1,307,380 kgf. Total Mass: 1,096,920 kg. Core Diameter: 4.6 m. Total Length: 63.0 m. Launch Price $: 33.00 million. in 1965 price dollars.
- Stage Number: 0. 2 x Titan UA1207 Gross Mass: 319,330 kg. Empty Mass: 51,230 kg. Thrust (vac): 725,732 kgf. Isp: 272 sec. Burn time: 120 sec. Isp(sl): 245 sec. Diameter: 3.1 m. Span: 3.1 m. Length: 34.1 m. Propellants: Solid No Engines: 1. UA1207
- Stage Number: 1. 1 x Titan LDC-1 Gross Mass: 350,000 kg. Empty Mass: 20,000 kg. Thrust (vac): 443,012 kgf. Isp: 296 sec. Burn time: 210 sec. Isp(sl): 258 sec. Diameter: 4.6 m. Span: 4.6 m. Length: 29.9 m. Propellants: N2O4/Aerozine-50 No Engines: 4. LR-87-7
- Stage Number: 2. 1 x Titan LDC-2 Gross Mass: 50,000 kg. Empty Mass: 3,000 kg. Thrust (vac): 45,359 kgf. Isp: 316 sec. Burn time: 320 sec. Isp(sl): 160 sec. Diameter: 4.6 m. Span: 4.6 m. Length: 13.4 m. Propellants: N2O4/Aerozine-50 No Engines: 1. LR-91-7
- Stage Number: 3. 1 x Centaur D/E Gross Mass: 16,258 kg. Empty Mass: 2,631 kg. Thrust (vac): 13,381 kgf. Isp: 444 sec. Burn time: 470 sec. Isp(sl): 0 sec. Diameter: 3.1 m. Span: 3.1 m. Length: 9.6 m. Propellants: Lox/LH2 No Engines: 2. RL-10A-3
Bibliography:- 223 - Titan Marketing Brochure, Martin Company, 1967.
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Last update 12 March 2001.
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© Mark Wade, 2001 .