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

Focke-Wulf A 20 Habicht

From Wikipedia, the free encyclopedia

A 20 Habicht
Role Airliner
Manufacturer Focke-Wulf
First flight 1927
Number built 4

The Focke-Wulf A 20 Habicht (German: "Hawk") was an airliner developed in Germany in the late 1920s. It was a high-wing cantilever monoplane with fixed tailskid undercarriage. The fuselage was deep and seated four passengers in a fully enclosed cabin. The type was not bought by the airlines and only a few examples were built.

Variants

A.20
standard version with Mercedes D.II engine.
A.20a
one-off version with Wright Whirlwind engine, for export.
A.28
version with Bristol Titan engine.

Specifications (A.20)

Data from Jane's all the World's Aircraft 1928[1]

General characteristics

  • Crew: 1
  • Capacity: 3 or 4 passengers
  • Length: 10.2 m (33 ft 6 in)
  • Wingspan: 16 m (52 ft 6 in)
  • Height: 3 m (9 ft 10 in)
  • Wing area: 32 m2 (340 sq ft)
  • Empty weight: 988 kg (2,178 lb)
A.20a 1,000 kg (2,200 lb)
  • Gross weight: 1,425 kg (3,142 lb)
A.20a 1,600 kg (3,500 lb)
  • Powerplant: 1 × Mercedes D.IIa 6-cylinder water-cooled in-line piston engine, 89 kW (120 hp)
A.20a 1x Wright Whirlwind 9-cylinder air-cooled radial piston engine 150 kW (200 hp)
  • Propellers: 2-bladed fixed pitch propeller

Performance

  • Maximum speed: 145 km/h (90 mph, 78 kn)
A.20a 170 km/h (110 mph; 92 kn)
A.20a Cruising speed 150 km/h (93 mph; 81 kn)
A.20a Landing speed 80 km/h (50 mph; 43 kn)
  • Service ceiling: 3,500 m (11,500 ft)
  • Time to altitude: 1,000 m (3,300 ft) in 10 minutes
A.20a 1,000 m (3,300 ft) in 5.4 minutes
  • Wing loading: 44.5 kg/m2 (9.1 lb/sq ft)
A.20a 50 kg/m2 (10 lb/sq ft))
A.20a 0.1021 kW/kg (0.0621 hp/lb))

References

  1. ^ Grey, C.G., ed. (1928). Jane's all the World's Aircraft 1928. London: Sampson Low, Marston & company, ltd. p. 136c.

Further reading

External links

This page was last edited on 11 February 2024, at 23:02
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.