Jump to content

Caspar CLE 11

Edit links
From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by Cydebot (talk | contribs) at 04:08, 8 May 2019 (Robot - Moving category German airliners 1920–1929 to Category:1920s German airliners per CFD at Wikipedia:Categories for discussion/Log/2019 April 19.). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

The Caspar CLE 11 was an airliner built in Germany in the early 1920s.

Development

Only one CLE 11 was built (registration D-294), and it took part in the International Air Exhibition in Gothenburg (Sweden) in July 1923.[1]

Specifications

Data from [1]

General characteristics

  • Crew: One
  • Capacity: 2 passengers
  • Length: 6.72 m (22 ft 1 in)
  • Wingspan: 12.00 m (39 ft 4 in)
  • Height: 2.20 m (7 ft 3 in)
  • Wing area: 19.00 m2 (204.5 sq ft)
  • Empty weight: 450 kg (992 lb)
  • Gross weight: 830 kg (1,830 lb)
  • Powerplant: 1 × Siemens-Halske Sh 5 5-cylinder air-cooled radial piston engine, 60 kW (80 hp)
  • Propellers: 2-bladed fixed pitch propeller

Performance

  • Maximum speed: 160 km/h (99 mph, 86 kn)
  • Cruise speed: 145 km/h (90 mph, 78 kn)
  • Range: 800 km (500 mi, 430 nmi)
  • Endurance: 6 hours
  • Service ceiling: 3,000 m (9,800 ft)

References

  1. ^ a b "Caspar CLE 11". Histaviation.com. Retrieved 27 February 2019.


Stub icon

This article on an aircraft of the 1920s is a stub. You can help Wikipedia by expanding it.

Retrieved from "https://en.wikipedia.org/w/index.php?title=Caspar_CLE_11&oldid=896059096"