Engine Model: 200 inch solid, segment x 4. Propellants: Solid. Thrust(vac): 11,120.000 kN (2,499,870 lbf). Isp: 285 sec. Burn time: 175 sec. Diameter: 5.20 m (17.00 ft). Length: 35.10 m (115.10 ft). Chambers: 1. Country: USA. Status: Study 1960. 4 used as first stage of solid Nova design. Extended high-expansion nozzles. Specific impulse based on UA1205 solid motors of same period. Masses estimated based on total vehicle thrust, performance, and stage volumes.
200 inch solid, segment x 4 used on Rocket Stages