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XLR20AJ-2
Aerojet Nitric acid/Gasoline rocket engine. Development begun January 1946. Blast turbine, three levels of thrust (600/1000/7500 lbf). Replaced NM Lark.

AKA: XLR20-AJ-2. Date: January 1946. Thrust: 6.66 kN (1,497 lbf).

Thrust (sl): 6.660 kN (1,497 lbf). Thrust (sl): 680 kgf. Propellant Formulation: WFNA/Gasoline.

Family: Storable liquid. Country: USA. Launch Vehicles: Lark. Propellants: Nitric acid/Gasoline. Agency: Aerojet.
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