Zeppelin-Lindau C.I

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Zeppelin-Lindau C.I
Role Experimental
Manufacturer Zeppelin-Lindau
Designer Claude Dornier
First flight March 1917
Number built 9
Variants Zeppelin-Lindau C.II

The Zeppelin Lindau C.I was a German single-engine two-seat biplane, designed by Claude Dornier and built by Zeppelin Lindau in World War II.[1] Intended to investigate stressed-skin construction, it had an all-metal fuselage in which the Aluminium alloy skin was load bearing; the wings had aluminium alloy box spars but were fabric covered

Specifications (variant specified)[]

Data from [2]

General characteristics

  • Crew: 2
  • Length: 7.42 m (24 ft 4 in)
  • Wingspan: 10.5 m (34 ft 5 in)
  • Height: 2.76 m (9 ft 1 in)
  • Wing area: 25.82 m2 (277.9 sq ft)
  • Empty weight: 728 kg (1,605 lb)
  • Gross weight: 1,068 kg (2,355 lb)
  • Powerplant: 1 × Mercedes D.III 6-cylinder in-line water-cooled piston engine, 120 kW (160 hp)
  • Propellers: 2-bladed fixed-pitch wooden propeller

Performance

  • Maximum speed: 150 km/h (93 mph, 81 kn)
  • Time to altitude: 1,000 m (3,300 ft) in 4 minutes 30 seconds; 3,000 m (9,800 ft) in 18 minutes; 5,000 m (16,000 ft) in 60 minutes 24 seconds

Armament

  • Guns: 1x fixed forward-firing 7.92 mm (0.312 in) MG08 Spandau machine-gun and 1x flexibly mounted 7.92 mm (0.312 in) Parabellum MG14 machine gun

References[]

  1. ^ Forsyth, Robert; Luijken, Wiek (Illustrator); Tooby, Adam (Illustrator); Schatz, Simon (Illustrator) (18 Oct 2018). Dornier Do 335: X-Planes 9. Osprey Publishing. ISBN 9781472828897.
  2. ^ Gray, Peter; Thetford, Owen (1970). German Aircraft of the First World War (2nd ed.). London: Putnam. p. 577. ISBN 0-370-00103-6.
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