X4-AL-1000

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X4-AL-1000

Part of LR53 engine series

Aerojet Nitric acid/Amine rocket engine. Braking rocket for glider. Single uncooled chamber, pressure fed, 13 kg of propellant.

AKA: XLR9-AJ-1. Thrust: 4.41 kN (991 lbf). Burn time: 4.00 s. Height: 1.07 m (3.51 ft). Diameter: 0.36 m (1.18 ft).

Thrust (sl): 4.410 kN (991 lbf). Thrust (sl): 450 kgf. Engine: 367 kg (809 lb). Chamber Pressure: 18.70 bar. Propellant Formulation: RFNA/Aniline.

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

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