Gloster F.9/37

Airplanes

Length

11.2776 m

Flat Wing Span

15.24 m

Height

3.3528 m

Flat Wing Area

35.8606 m²

Max Speed

579.3638 km/h

Max Ceiling

9144 m

Number of Engines

First Flight

1939-04-03

Number Built

Pictures

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Aircraft
Gloster F.9/37

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Rogožarski SIM-XIV-H		11.2	15.2		Compare
Mikoyan-Gurevich DIS	Mikulin AM-37	11.2	15.3		Compare
Focke-Wulf Fw 187 Falke		11.1	15.3		Compare
Aero Commander 500 family		11.22	14.95		Compare
Miles Aerovan	Blackburn Cirrus Major	10.9728	15.24	10	Compare
Potez 220	Gnome-Rhône 14M	10.9728	15.24		Compare

All data (20 fields)

Name: Gloster F.9/37
Manufacturer: Gloster Aircraft Company
Description: The Gloster F.9/37, also known as the Gloster G.39, was a British twin-engined design from the Gloster Aircraft Company for a cannon-armed heavy fighter to serve with the Royal Air Force, planned before the Second World War.
First Flight: 1939-04-03
Designer: George Carter
Type: Heavy fighter
Length (m): 11.2776
Height (m): 3.3528
Cockpit Crew: 1
Max Speed (km/h): 579.3638
Max Ceiling (m): 9144
Rate of Climb (m/s): 12.4968
Armament: :* Four 0.303 in (7.7 mm) Browning machine guns :* Two 20 mm Hispano cannon; :*provision for 20 lb bomb carriers
Number Built: 2
Powerplant Description: 2 × Bristol Taurus T-S(a) 14-cylinder air-cooled sleeve-valve radial piston engines, 746 kW (1000 hp) each
Primary Users: Royal Air Force (intended)
Wikipedia Article (URL): en.wikipedia.org/wiki/Gloster_F.9/37
Flat Wing Span (m): 15.24
Flat Wing Area (m²): 35.8606
Number of Engines: 2