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Pershing 2 St1
Part of Pershing 2 Family
Thiokol, Hercules solid rocket engine. Pershing 2 first stage.

AKA: Pershing 2-1. Status: Retired 1988. Thrust: 172.00 kN (38,667 lbf). Gross mass: 4,100 kg (9,000 lb). Unfuelled mass: 530 kg (1,160 lb). Burn time: 58 s. Height: 4.00 m (13.10 ft). Diameter: 1.02 m (3.34 ft).



Country: USA. Launch Vehicles: Pershing 2. Propellants: Solid. Stages: Pershing 2 St1. Agency: Thiokol, Hercules.

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