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TX-175
Thiokol solid rocket engine. Pershing 1A second stage.

AKA: Pershing 1A-2. Status: Retired 1983. Thrust: 85.00 kN (19,108 lbf). Gross mass: 2,000 kg (4,400 lb). Burn time: 39 s. Height: 2.70 m (8.80 ft). Diameter: 1.02 m (3.34 ft).



Country: USA. Launch Vehicles: Pershing 1, Pershing 1A. Propellants: Solid. Stages: TX-175. Agency: Thiokol, Martin.

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