200 inch solid segment x 6

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200 inch solid segment x 6

Notional solid rocket engine. NASA Nova study 1960. 5 used as first stage of solid Nova design. Solid propellant rocket stage. 5 used as first stage of solid Nova design. Masses estimated based on total vehicle thrust, performance, and stage volumes.

AKA: Nova Solid 6. Status: Study 1960. Thrust: 28,017.00 kN (6,298,472 lbf). Specific impulse: 263 s. Specific impulse sea level: 238 s. Burn time: 97 s. Height: 45.70 m (149.90 ft). Diameter: 5.20 m (17.00 ft).

Specific impulse based on UA1205 solid motors of same period. Masses estimated based on total vehicle thrust, performance, and stage volumes.

Country: USA. Launch Vehicles: Nova 5S. Propellants: Solid.

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