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45AL-2600
Part of AJ11 engine series
Aerojet Nitric acid/Amine rocket engine. Development begun June 1948. Manufacture of complete Aerobee systems First flight 1955.

Date: June 1948. Thrust: 11.70 kN (2,630 lbf).

Thrust (sl): 11.700 kN (2,630 lbf). Thrust (sl): 1,200 kgf. Propellant Formulation: RFNA/Aniline+Furfural Alcohol.



Family: Storable liquid. Country: USA. Launch Vehicles: Aerobee Hi. Propellants: Nitric acid/Amine. Agency: Aerojet.

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