Star 26B (original) (raw)

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Star 26B

Part of Star 26

Star-26B
Credit: Thiokol

Thiokol solid rocket engine. In Production. Upper stage motor flown on the Burner IIA spacecraft for Boeing and the U.S. Air Force.

AKA: 17.8-KS-7,784;Burner 2A;TE-M-442-1. Status: In Production. Thrust: 34.63 kN (7,784 lbf). Gross mass: 261 kg (575 lb). Unfuelled mass: 23 kg (50 lb). Specific impulse: 272 s. Burn time: 18 s. Diameter: 0.66 m (2.17 ft).

Total flown included in total for Star-26C. Total impulse 64,731 kgf-sec. Motor propellant mass fraction 0.91.

Country: USA. Launch Vehicles: Thor Burner 2A. Propellants: Solid. Stages: Star 26B. Agency: Thiokol. Bibliography: 410.

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