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TX-174
Thiokol solid rocket engine. Pershing 1A first stage.

AKA: Pershing 1A-1. Status: Retired 1983. Thrust: 117.00 kN (26,302 lbf). Gross mass: 2,000 kg (4,400 lb). Burn time: 39 s. Height: 2.80 m (9.10 ft). Diameter: 1.02 m (3.34 ft).



Country: USA. Launch Vehicles: Pershing 1, Pershing 1A. Propellants: Solid. Stages: TX-174. Agency: Thiokol, Martin.

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