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X60AL-1300
Aerojet Nitric acid/Amine rocket engine. Development begun January 1945. Superperformance

Date: January 1945. Thrust: 5.78 kN (1,299 lbf).

Thrust (sl): 5.780 kN (1,299 lbf). Thrust (sl): 590 kgf. Propellant Formulation: RFNA/Aniline+Furfural Alcohol.

Family: Storable liquid. Country: USA. Propellants: Nitric acid/Amine. Agency: Aerojet.
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