The Gnome-Rhône 14M was a small 14-cylinder two-row air-cooled radial engine that was used on several French and German aircraft of World War II.
14M-00LH rotation, 474 kW (635 hp)
14M-01RH rotation identical to 14M-00
14M-04LH rotation, 521.99 kW (700 hp)
14M-05RH rotation identical to 14M-04
14M-06LH rotation, 521.99 kW (700 hp), reduction gear 0.71:1
14M-07RH rotation identical to 14M-06
14M-08LH rotation, 559.27 kW (750 hp), reduction gear 0.71:1
14M-09RH rotation identical to 14M-08
Breguet 693Focke-Wulf Fw 189EGotha Go 244SNCAC NC.510MSNCAC NC.530SNCAC NC.600Henschel Hs 129BPotez 631Potez 633Potez 637Potez 662Potez 63.11(14M-5 identical except opposite rotation)
Data from
Type: Fourteen-cylinder two-row supercharged air-cooled radial engineBore: 122 mm (4.80 in)Stroke: 116 mm (4.57 in)Displacement: 18.92 L (1,154.6 cu in)Length: 1,251 mm (49.25 in)Diameter: 950 mm (37.40 in)Dry weight: 419 kg (924 lb)Valvetrain: Two overhead valves per cylinderSupercharger: gear driven, 8.258:1 ratio, 1-speed superchargerFuel system: Bronzavia 110-L2 carburretor with automatic boost and altitude controlFuel type: 87 octane rating gasolineOil system: Pressure feed 482.6 kPa (70 psi), dry sump, 120 S.U. secs (25.1 cSt) grade oil.Cooling system: Air-cooledReduction gear: 0.71:1Air Equipment 47 electric inertia starterPower output:
(Take-off): 521.99 kW (700 hp) at 3,030 rpm for takeoff with 1,100 mm (43.3 in) Hg / +3 kg (6.6 lb) boost(Normal): 492.16 kW (660 hp) at 3,030 rpm at 4,000 m (13,123 ft)(cruising): 339.29 kW (455 hp) at 2,350 rpm at 4,000 m (13,123 ft)Specific power: 27.21 kW/l (0.61 hp/(cu in))Compression ratio: 6.5:1Specific fuel consumption: 0.29 kg/(kW h) (0.48 lb/(hp h))Oil consumption: 0.01 kg/(kW h) (0.018 lb/(hp h))Power-to-weight ratio: 1.27 kW/kg (0.77 hp/lb)B.m.e.p. max: 1,075 kPa (155.9 psi)