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MIM-14A

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AKA: Nike Hercules;SAM-A-25;W31. Payload: 510 kg (1,120 lb). Thrust: 775.00 kN (174,226 lbf). Gross mass: 4,530 kg (9,980 lb). Height: 12.50 m (41.00 ft). Diameter: 0.79 m (2.59 ft). Span: 2.29 m (7.51 ft). Apogee: 46 km (28 mi).

Development Cost $: 148.700 million. Recurring Price $: 0.195 million in 1964 dollars. Flyaway Unit Cost 1985$: 0.055 million in 1964 dollars. Maximum range: 139 km (86 mi). Number Standard Warheads: 1. Standard warhead: W31. Warhead yield: 40 KT. Boost Propulsion: Solid rocket. Maximum speed: 4,190 kph (2,600 mph). Initial Operational Capability: 1958. Total Number Built: 9302. Total Development Built: 302. Total Production Built: 9000. Floor: 600 m (1,960 ft). Surveillance Radar: FP-37. Tracking Radar: FP-36.