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Caproni CH.1

Military Aircraft

The Caproni CH.1 was a single-seat biplane fighter, of which a single prototype was produced in Italy in 1935. Antonio Chiodi began design work in 1934 as a private venture of the Caproni company, and the CH stood for Chiodi. He designed it as an aerodynamically clean single-bay biplane of all-metal construction with fabric skin and wings of equal span, spatted landing gear and an enclosed cockpit under a canopy that slid to the rear. Chiodi intended a Gnome-Rhone 14K Mistral Major radial engine, but the aircraft was built with a 417 kilowatt Piaggio Stella P.IX nine-cylinder radial. Chiodi himself flew it on its first flight in May 1935. The Regia Aeronautica placed no production order and no further examples were built. The listed figures are a length of 7.19 metres, a wingspan of 8.6 metres, an empty mass of 1,400 kilograms and a best speed of 377 kilometres per hour at 5,000 metres.

Facts
Year
1935 1
Units Built
1 1
Top Speed (km/h)
377 1
Mass (kg)
1400 1
Maximum Mass (kg)
2000 1
Engine
Piaggio Stella P.IX R.C.40 9-cylinder radial engine 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Caproni CH.1 (Wikipedia)

Of Make

Source Caproni CH.1 (Wikipedia)
Sources
1. Caproni CH.1 (Wikipedia)
  • Lead
    was a single-seat biplane fighter
  • Operational history
    which took place in May 1935
  • Lead, units built
    a single example of which was produced as a prototype in Italy in 1935
  • Specifications (CH.1)
    1 × Piaggio Stella P.IX R.C.40 9-cylinder radial
  • Specifications (CH.1), top speed
    377 km/h (234 mph; 204 kn) at 5,000 m (16,000 ft)
  • Specifications (CH.1), mass
    Empty weight: 1,400 kg (3,086 lb)
  • Specifications (CH.1), maximum mass
    Gross weight: 2,000 kg (4,409 lb)
  • Design
    as a private venture of the Caproni company
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