To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

4,5
Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
Languages
Recent
Show all languages
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.
.
Leo
Newton
Brights
Milds

Gourdou-Leseurre GL.50

From Wikipedia, the free encyclopedia

GL-50
Role Fighter
National origin France
Manufacturer Gourdou-Leseurre
First flight 1922
Number built 2

The Gourdou-Leseurre GL.50, also known as the Gourdou-Leseurre Type F, was a French fighter prototype of the early 1920s.

Development

In April 1919, General Duval of the French Armée de l'Air set out for the replacement of two of the principal categories of aircraft within the air force - CAP2 (Chasse, Armée, Biplace meaning 'armed two-seat fighter') and CAN2 (Chasse, Armée, Nuit, Biplace meaning 'armed two-seat night fighter'). Gourdou-Leseurre put forward the GL-50 as a submission for the CAP2 category (despite the fact that this categorisation system was removed in 1920). Its 300 hp Hispano-Suiza engine was intended to be fitted with a supercharger, however this was not fitted, despite the fact it would have increased its performance drastically. It was of wooden construction, with a long-span untapered wing, considered unusual at the time, that feature being more in line with single-seat aircraft design, as were the wing bracing struts.

Operational history

The date is not recorded of the first flight of the GL-50, however it is known that it occurred in 1922. However, for no apparent reason the aircraft did not satisfy the needs of the specification and therefore no further production was continued. Only 1 GL.50 was built, and also one of its main variant, the GL.51.

Variants

  • GL.51 - intended to satisfy the CAN2 specification. Similar to the GL-50 except for a 380 hp Gnome & Rhône 9Ab engine and a lighter loaded weight resulting in a higher top speed


Specifications (GL.50)

General characteristics

  • Crew: 2
  • Length: 9.3505 m (30 ft 8.13 in)
  • Wingspan: 14.60 m (47 ft 11 in)
  • Height: 2.85 m (9 ft 4 in)
  • Wing area: 40.00 m2 (430.57 sq ft)
  • Gross weight: 2,010 kg (4,431 lb)
  • Powerplant: 1 × Hispano-Suiza 8Fb , 224 kW (300 hp)

Performance

  • Maximum speed: 210 km/h (131 mph, 114 kn)

Armament

  • 2 x fixed forward-firing 7.7mm Darne machine gun
  • 2 x rear-mounted swivelling 7.7mm Darne machine gun

References

  • Green, William; Gordon Swanborough. The Complete Book of Fighters. Godalming, UK: Salamander Books. p. 254.
This page was last edited on 16 April 2021, at 21:35
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.