• Source: Caspar C 30
    • The Caspar C 30, aka Caspar LE 30 was an aerial reconnaissance aircraft developed in Germany and built in Denmark in the late 1920s.


      Design and development


      It was a single-bay biplane with staggered, equal-span wings.


      Specifications


      Data from General characteristics
      Crew: 2
      Length: 9.1 m (29 ft 10 in)
      Wingspan: 10.8 m (35 ft 5 in)
      Empty weight: 1,200 kg (2,646 lb)
      Gross weight: 1,700 kg (3,748 lb)
      Powerplant: 1 × Hispano-Suiza 12Jb V-12 water-cooled piston engine, 280 kW (380 hp)
      Propellers: 2-bladed fixed pitch propeller
      Performance

      Maximum speed: 240 km/h (150 mph, 130 kn)
      Cruise speed: 205 km/h (127 mph, 111 kn)
      Range: 1,000 km (620 mi, 540 nmi)
      Service ceiling: 7,000 m (23,000 ft)


      References




      Further reading


      Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 239. ISBN 978-0517691861.

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