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||Liquid-cooled V-12 piston engine
The Packard 1A-1500 was an American 12-cylinder liquid-cooled 60-degree Vee piston aircraft engine designed in 1924. Test flown in the second prototype Douglas XO-2 it proved to be unreliable. Only 29 engines were built.
Data from STATISTICS OF ALL THE AERO ENGINES OF PACKARD
- Power output: 500 hp (370 kW) at 2,000 rpm maximum continuous;520 hp (390 kW) at 2,200 rpm for takeoff
- Specific power: 0.347 hp/cu in (15.8 kW/l)
- Power-to-weight ratio: 0.722 hp/lb (1.187 kW/kg)