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| | SSM-N-8 Regulus - Wikipedia, the free encyclopedia |
 | | In August 1947, the specifications for the project, now named "Regulus," were issued: carry a 3,000 pound (1,360 kg) warhead, to a range of 500 nautical miles (926 km), at Mach 0.85, with a circular error probable (CEP) of 0.5 percent of the range. |
 | | RAM converted the Regulus cruise missiles into an unmanned aerial vehicle (UAV): Regulus missiles would be launched from cruisers or submarines, and once in flight, guided to their targets by carrier based pilots with remote control equipment. |
 | | A second generation supersonic Regulus II cruise missile with a range of 1,200 nautical miles (2,200 km) and a speed of Mach 2 was developed and successfully tested, but the program was canceled in favor of the Polaris ballistic nuclear missile. |
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