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SSM-N-8 Regulus

The SSM-N-8A Regulus or the Regulus I was a United States Navy-developed ship-and-submarine-launched, nuclear-capable turbojet-powered second generation cruise missile, deployed from 1955 to 1964. Wikipedia
Engine: Allison J33-A-14 turbojet 4,600 lbf (20 kN); 2 × booster rockets 33,000 lbf (150 kN)
Manufacturer: Chance Vought
Maximum speed: Subsonic
Operational range: 500 nautical miles (926 km)
Warhead: 3,000 pounds (1,400 kg) such as the W5 warhead or the W27 warhead