UA1206 (original) (raw)

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UA1206

Part of UA1200

CSD solid rocket engine. Used on Titan 34D launch vehicle. First flight 1982.

AKA: Titan UA1206. Status: Retired 1992. Number: 38 . Thrust: 6,226.90 kN (1,399,863 lbf). Gross mass: 251,427 kg (554,301 lb). Unfuelled mass: 40,827 kg (90,008 lb). Specific impulse: 265 s. Specific impulse sea level: 240 s. Burn time: 114 s. Height: 27.56 m (90.41 ft). Diameter: 3.05 m (10.00 ft).

Thrust (sl): 5,639.500 kN (1,267,810 lbf). Thrust (sl): 575,074 kgf. Propellant Formulation: PBAN.

Country: USA. Launch Vehicles: Titan 34D/IUS, Titan 34D, Titan 34D/Transtage, Commercial Titan 3. Propellants: Solid. Stages: UA1206. Agency: CSD.

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