AJ-260X 1/3

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AJ-260X 1/3

Part of AJ-260

Aerojet solid rocket engine. Design concept 1960's. Solid propellant rocket stage. 260 inch solid booster - full length. Saturn 3S second stage.

AKA: Saturn 3S-2. Status: Design concept 1960's. Thrust: 11,143.00 kN (2,505,046 lbf). Specific impulse: 263 s. Specific impulse sea level: 238 s. Burn time: 114 s. Height: 14.00 m (45.00 ft). Diameter: 6.60 m (21.60 ft).

Country: USA. Propellants: Solid. Stages: AJ-260X 1/3. Agency: Aerojet.

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