UA1205

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UA1205

Part of UA1200

CSD solid rocket engine. Out of production. Strap-on boosters for Titan 3C, 3D, 3E. Proposed for advanced Saturn IB versions. First flight 1965.

AKA: SR-47;Titan UA1205. Status: Out of production. Number: 130 . Thrust: 5,849.30 kN (1,314,975 lbf). Gross mass: 226,233 kg (498,758 lb). Unfuelled mass: 33,798 kg (74,511 lb). Specific impulse: 263 s. Specific impulse sea level: 238 s. Burn time: 115 s. Height: 25.91 m (85.00 ft). Diameter: 3.05 m (10.00 ft).

Thrust (sl): 5,293.300 kN (1,189,981 lbf). Thrust (sl): 539,775 kgf. Propellant Formulation: PBAN.

Country: USA. Launch Vehicles: Titan IIIC, Saturn MLV-V-4(S), Saturn MLV-V-4(S)-A, Saturn IB-D, Saturn INT-12, Saturn INT-16, Titan IIID, Titan 23C, Titan IIIE. Propellants: Solid. Stages: UA1205. Agency: CSD.

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