Kalpana Kalpana (Editor)

Sablatnig C.I

Updated on
Edit
Like
Comment
Share on FacebookTweet on TwitterShare on LinkedInShare on Reddit
Top speed
  
120 km/h

Length
  
8.7 m

Wingspan
  
16 m

Manufacturer
  
Sablatnig

Sablatnig C.I httpsuploadwikimediaorgwikipediacommonsthu

The Sablatnig C.I was a conventional C-type reconnaissance two-seater aircraft developed and built by Sablatnig in Berlin, Germany in 1917. It was a two-bay biplane of conventional design, with staggered wings, two open cockpits in tandem, and fixed, tailskid undercarriage.

The C.I was developed into the Sablatnig N.I in 1918.

Specifications

General characteristics

  • Length: 8.7 m (28 ft 7 in)
  • Wingspan: 16.0 m (52 ft 6 in)
  • Empty weight: 1,050 kg (2,315 lb)
  • Gross weight: 1,540 kg (3,395 lb)
  • Powerplant: 1 × Argus As III , 130 kW (180 hp)
  • Propellers: 2-bladed

    • Performance

  • Maximum speed: 120 km/h (75 mph; 65 kn)
  • Time to altitude: 9 min to 3,281 ft (1,000 m)

    • Armament

  • Guns: 1 x Parabellum machine-gun
  • Bombs: 6 x 110 lb (50 kg) bombs

    • References

    Sablatnig C.I Wikipedia
    (Text) CC BY-SA