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Engine Model: 280 inch solid. Propellants: Solid. Thrust(vac): 46,208.000 kN (10,387,971 lbf). Isp: 265 sec. Isp (sea level): 238 sec. Burn time: 118 sec. Diameter: 7.10 m (23.20 ft). Length: 52.80 m (173.20 ft). Chambers: 1. Country: USA. Status: Study 1963. Operational date would have been February 1973 280 inch solid used on Rocket Stages
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