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Trident Motor
Philco-Ford solid rocket engine. Atlas F/Trident second stage.

AKA: Atlas F/Trident-2. Status: Retired 1971. Thrust: 35.00 kN (7,868 lbf). Gross mass: 1,100 kg (2,400 lb). Unfuelled mass: 700 kg (1,540 lb). Height: 2.00 m (6.50 ft). Diameter: 2.13 m (6.98 ft).



Country: USA. Launch Vehicles: Atlas F/Trident, Atlas E/Trident. Propellants: Solid. Stages: Trident Motor.

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