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AJ-260-1/3
Part of AJ-260 Family
Aerojet solid rocket engine. Design concept 1960's. Used on Saturn INT-05B launch vehicle. Solid propellant rocket stage. Study NASA 1969.

AKA: 260 inch solid TL. Status: Design concept 1960's. Thrust: 10,105.00 kN (2,271,694 lbf). Specific impulse: 275 s. Burn time: 130 s. Height: 14.00 m (45.00 ft). Diameter: 6.60 m (21.60 ft).

Country: USA. Launch Vehicles: Saturn INT-05A. Propellants: Solid. Stages: AJ-260-1/3. Agency: Aerojet.



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