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X60ALD-4000

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AKA: XLR13-AJ-1. Date: May 1946. Thrust: 17.60 kN (3,957 lbf). Unfuelled mass: 363 kg (800 lb). Burn time: 60 s. Height: 3.43 m (11.25 ft). Diameter: 0.81 m (2.65 ft).

Later redesigned to use WFNA and gasoline.

Thrust (sl): 17.600 kN (3,957 lbf). Thrust (sl): 1,800 kgf. Engine: 363 kg (800 lb). Chamber Pressure: 21.00 bar. Propellant Formulation: RFNA/80% Aniline+20% Furfural Alcohol.