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Star 48A s
Part of Star 48 Family
Star-48A Short
Star-48A Short
Credit: Thiokol
Thiokol solid rocket engine. In Production. Short nozzle upper-stage motor designed to fit within the dimensional envelope of the long nozzle.

AKA: 87.2-KS-17,335; TE-M-799-1. Status: In Production. Thrust: 77.11 kN (17,335 lbf). Gross mass: 2,574 kg (5,674 lb). Unfuelled mass: 144 kg (317 lb). Specific impulse: 283 s. Burn time: 87 s. Diameter: 1.24 m (4.08 ft).

Total flown included in total for Star-48A-l. Total impulse 693,030 kgf-sec. Motor propellant mass fraction 0.944.

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



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