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

Albatros D.XII

From Wikipedia, the free encyclopedia

Albatros D.XII
Role Fighter
Manufacturer Albatros Flugzeugwerke
First flight March 1918
Status retired
Primary user Germany
Number built 2

The Albatros D.XII was a German single-seat fighter biplane first flown in March 1918. It was the last of the Albatros fighters completed and flown before the end of World War I and had the same slab-sided fuselage seen on the Albatros D.X.

Design and development

The first example of the D.XII used a 134 kW (180 hp) Mercedes D.IIIa engine and had balanced, parallel-chord ailerons. The second, built in April 1918, featured unbalanced, inversely tapered ailerons and Bohme undercarriage with pneumatic shock absorbers. Although it was initially fitted with the Mercedes engine, it was later re-engined with a BMW IIIa producing 138 kW (185 hp). In this form, the D.XII competed in the third Adlershof D-Type Contest in October 1918. No further aircraft were built.

Specifications (D.XII)

Data from German Aircraft of the First World War.[1]

General characteristics

  • Crew: 1
  • Length: 5.785 m (19 ft 0 in)
  • Wingspan: 8.2 m (26 ft 11 in)
  • Height: 2.8 m (9 ft 2 in)
  • Wing area: 19.84 m2 (213.6 sq ft)
  • Empty weight: 580 kg (1,279 lb)
  • Gross weight: 760 kg (1,676 lb)
  • Powerplant: 1 × Mercedes D.III 6-cyl. water-cooled in-line piston engine, 120 kW (160 hp) (first prototype)
    • second prototype - 1x BMW IIIa 6-cyl.water-cooled in-line piston engine developing 138 kW (185hp)

Performance

  • Maximum speed: 180 km/h (110 mph, 97 kn)
  • Endurance: 1 hour
  • Rate of climb: 2.47 m/s (486 ft/min)
  • Time to altitude: 8,000 m (26,247 ft) in 54 minutes

Armament

Notes

  1. ^ Gray, Peter; Owen Thetford (1970). German Aircraft of the First World War (2nd ed.). London: Putnam & Company Ltd. ISBN 0-370-00103-6.

References

  • Gray, Peter; Owen Thetford (1970). German Aircraft of the First World War (2nd ed.). London: Putnam & Company Ltd. ISBN 0-370-00103-6.
  • Green, William; Gordon Swanborough (September 1995). The Complete Book of Fighters (1st ed.). Smithmark. ISBN 978-0-8317-3939-3.
This page was last edited on 24 January 2024, at 12:06
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.