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23KS11000
Part of Alcor
Aerojet solid rocket engine.

AKA: Alcor IA. Status: Retired 1974. Thrust: 49.00 kN (11,015 lbf). Gross mass: 500 kg (1,100 lb). Unfuelled mass: 200 kg (440 lb). Burn time: 23 s. Height: 1.90 m (6.20 ft). Diameter: 0.52 m (1.70 ft).



Country: USA. Launch Vehicles: Athena H. Propellants: Solid. Stages: 23KS11000. Agency: Aerojet.

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