| Titan UA1200 |
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Model: Titan UA1205. Gross Mass: 226,233 kg (498,758 lb). Empty Mass: 33,798 kg (74,511 lb). Thrust (vac): 5,849.411 kN (1,315,000 lbf). Isp: 263 sec. Burn time: 115 sec. Propellants: Solid. Isp(sl): 238 sec. Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft). Length: 25.91 m (85.00 ft). Country: USA. No Engines: 1. Motor: UA1205. Status: Study 1966. Cost $ : 17.980 million. First Flight: 1959. Last Flight: 1982. No Launched: 338.
Model: Titan UA1207. Gross Mass: 319,330 kg (704,000 lb). Empty Mass: 51,230 kg (112,940 lb). Thrust (vac): 7,116.999 kN (1,599,965 lbf). Isp: 272 sec. Burn time: 120 sec. Propellants: Solid. Isp(sl): 245 sec. Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft). Length: 34.14 m (112.00 ft). Country: USA. No Engines: 1. Motor: UA1207. Status: Study 1988. Cost $ : 24.360 million. First Flight: 1965. Last Flight: 1998. No Launched: 94. No Failed: 1.
Model: Titan UA1206. Gross Mass: 251,427 kg (554,301 lb). Empty Mass: 40,827 kg (90,008 lb). Thrust (vac): 6,226.997 kN (1,399,885 lbf). Isp: 265 sec. Burn time: 114 sec. Propellants: Solid. Isp(sl): 240 sec. Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft). Length: 27.56 m (90.41 ft). Country: USA. No Engines: 1. Motor: UA1206. Status: Retired 1992. Cost $ : 19.720 million. First Flight: 1982. Last Flight: 1992. No Launched: 62. No Failed: 1.
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