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Star 24A
Part of Star 24
Thiokol solid rocket engine. Out of Production. Total flown included in total for Star-24C. Total impulse 50,965 kgf-sec. Motor propellant mass fraction 0.903.

AKA: TE-M-604-2. Status: Out of Production. Gross mass: 198 kg (436 lb). Unfuelled mass: 19 kg (41 lb). Specific impulse: 282 s. Diameter: 0.62 m (2.04 ft).

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