21AL-2600

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21AL-2600

Part of AJ11 engine series

Aerojet Nitric acid/Amine rocket engine. Development begun January 1946. Regeneratively cooled. Development and production first flight 1953.

Date: January 1946. Thrust: 11.70 kN (2,630 lbf).

Thrust (sl): 11.700 kN (2,630 lbf). Thrust (sl): 1,200 kgf. Propellant Formulation: Nitric acid/Aniline.

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

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