Star 24C

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Star 24C

Part of Star 24

Star-24C
Credit: Thiokol

Thiokol solid rocket engine. In Production. Apogee motor designed and qualified for the NASA International Ultraviolet Experiment satellite.

AKA: 28-KS-4,825;TE-M-604-4. Status: In Production. Number: 15 . Thrust: 21.47 kN (4,826 lbf). Gross mass: 239 kg (526 lb). Unfuelled mass: 19 kg (41 lb). Specific impulse: 282 s. Burn time: 28 s. Diameter: 0.62 m (2.04 ft).

It incorporates a 1.5-inch longer cylindrical section with increased propellant weight and a larger nozzle throat and operates at a slightly higher chamber pressure than prior STAR 24 motors. Total impulse 62,573 kgf-s. Propellant mass fraction 0.917.

Country: USA. Propellants: Solid. Agency: Thiokol. Bibliography: 410.

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