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UA1207
Part of UA1200 Family
CSD seven-segment solid rocket engine, originally developed in the 1960's for the cancelled MOL project. First flight 1989.

AKA: Titan UA1207. Status: First flight 1989. Number: 44 . Thrust: 7,116.90 kN (1,599,943 lbf). Gross mass: 319,330 kg (704,000 lb). Unfuelled mass: 51,230 kg (112,940 lb). Specific impulse: 272 s. Specific impulse sea level: 245 s. Burn time: 120 s. Height: 34.14 m (112.00 ft). Diameter: 3.05 m (10.00 ft).

Thrust (sl): 6,410.400 kN (1,441,115 lbf). Thrust (sl): 653,692 kgf. Propellant Formulation: PBAN.



Country: USA. Launch Vehicles: Titan 3M, Titan 3L2, Titan 3L4, Titan 3C7, Saturn INT-11, Saturn INT-13, Saturn INT-18, Saturn V-ELV, Saturn MLV-V-4(S)-B, Titan 4, Barbarian MM, Titan 5, Titan 402A/IUS, Titan 405A, Titan 403A, Titan 404A, Titan 401A/Centaur. Propellants: Solid. Stages: UA1207. Agency: CSD.

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