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Antares 3A
Part of Antares Family
Thiokol solid rocket engine. Out of production. Used on Scout G launch vehicle. First flight 1979.

AKA: X-259A. Status: Out of production. Number: 17 . Thrust: 80.80 kN (18,165 lbf). Gross mass: 1,637 kg (3,608 lb). Unfuelled mass: 352 kg (776 lb). Specific impulse: 295 s. Burn time: 48 s. Height: 3.51 m (11.51 ft). Diameter: 0.76 m (2.49 ft).

Chamber Pressure: 48.00 bar. Area Ratio: 59.



Country: USA. Launch Vehicles: Scout G-1. Propellants: Solid. Stages: Antares 3A. Agency: Thiokol.

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