200 inch solid, segment x 6

Propellants: Solid. Thrust(vac): 28,017.000 kN (6,298,472 lbf). Isp: 263 sec. Isp (sea level): 238 sec. Burn time: 97 sec. Diameter: 5.20 m (17.00 ft). Length: 45.70 m (149.90 ft). Chambers: 1. Country: USA. Status: Study 1960.

Used in Nova 6 Segment. Status: Study, NASA, 1960.. 5 used as first stage of solid Nova design. 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 6 used on Rocket Stages

Used on stage: Nova Solid 6. on launch vehicle: Nova 5S.

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