325 in solid

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325 in solid

Notional solid rocket engine. Study 1963. Recoverable motors; separation at 1,972 m/s at 53,000 m altitude; splashdown using retrorockets under 3 61 m diameter parachutes 610 km downrange. Solid propellant rocket stage. Massed estimated based on tank volumes, total thrust, and first stage burnout conditions. Recoverable stage; separation at 1,972 m/s at 53,000 m altitude; splashdown using retrorockets under 3 61 m diameter parachutes 610 km downrange.

AKA: Nova GD-S. Status: Study 1963. Thrust: 69,047.00 kN (15,522,383 lbf). Specific impulse: 263 s. Specific impulse sea level: 238 s. Burn time: 116 s. Height: 60.40 m (198.10 ft). Diameter: 8.30 m (27.20 ft).

Masses estimated based on volumes, total thrust, and first stage burnout conditions.

Country: USA. Launch Vehicles: Nova GD-E. Propellants: Solid. Stages: 325 in solid.

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