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UA1207
Part of UA1200
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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