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Engine Model: 300 inch solid. Propellants: Solid. Thrust(vac): 63,595.000 kN (14,296,724 lbf). Isp: 263 sec. Isp (sea level): 234 sec. Burn time: 106 sec. Diameter: 7.60 m (24.90 ft). Length: 58.10 m (190.60 ft). Chambers: 1. Country: USA. Status: Study 1963. Operational date would have been April 1973 300 inch solid used on Rocket Stages
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