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TE-416
Thiokol solid rocket engine.

AKA: Tomahawk-2 Nike. Status: Retired 1995. Thrust: 53.00 kN (11,914 lbf). Gross mass: 200 kg (440 lb). Unfuelled mass: 60 kg (132 lb). Burn time: 9.50 s. Height: 3.50 m (11.40 ft). Diameter: 0.22 m (0.72 ft).

Country: USA. Launch Vehicles: Tomahawk, Nike Tomahawk, Terrier Tomahawk, D-Region Tomahawk, Sandhawk Tomahawk, Ute Tomahawk, Paiute Tomahawk, Taurus Tomahawk, Taurus Nike Tomahawk, Strypi Tomahawk. Propellants: Solid. Stages: TE-416. Agency: Thiokol.
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