Specifications – Fokker G.1

Crew: 2-3

Length: 10.87 m (35 ft 8 in)
Wingspan: 17.16 m (56.29 ft)
Height: 3.80 m (12.4 ft)
Wing area: 38.30 m² (412.26 ft²)
Empty weight: 3,325 kg (7,330 lb)
Loaded weight: 4,800 kg (10,582 lb)
Max. takeoff weight: 5,000 kg (11,023 lb)

Powerplant:
2 × Bristol Mercury VIII nine-cylinder air-cooled single-row piston radial engine
730 hp at 2,650 rpm for takeoff, 830 hp (618 kW) at 4,100m
at 2,750rpm maximum continuous power (545 kW) each

Performance:

Maximum speed: 475 km/h at 4,100m (295 mph)
Range: 1,510 km (938 mi)
Service ceiling: 10,000 m (32,808 ft)
Rate of Climb: 13.5 m/s (44.29 ft/s)
Power/mass: 0.22 kW/kg (0.14 hp/lb; 0.30 hp/kg)
Time to altitude: 6.0 min 20 sec to 5,000 m (16,405 ft)
Wing Loading: 125.3 kg/m² (25.68 lb/ft²)

Armament:
8× 7.9 mm (0.31 in) forward-firing FN-Browning machine guns in the nose
1× 7.9 mm (0.31 in) machine gun in rear turret
300 kg (660 lb) of bombs (G.1b could take 400 kg (880 lb))

Fokker G.1

Fokker G.1

Image Courtesy Wings Palette