Caproni Vizzola Calif

Source: Wikipedia, the free encyclopedia.
Calif
Role 2-seat Sailplane
Manufacturer
Caproni Vizzola
Designer Carlo Ferrarin and Livio Sonzio
First flight 1969

The Caproni Vizzola Calif was a family of Italian

chord and trapezoidal outer panels. The forward fuselage was constructed of fibreglass over an alloy frame, while the rear fuselage, wings, and empennage
were metal-covered.

The most significant member of the family, and the only one produced in quantity (around 150 by the early 1980s) was the A-21S, a two-seat version that accommodated the pilot and passenger side by side. At one time this aircraft concurrently held four world records for two-seat sailplanes, including:

Variants

  • A-10 (one built)
  • A-12 (two built)
  • A-14 (one built)
  • A-15 (one built)
  • A-20
    • A-20S - two-seat version of A-20
  • A-21 - two-seat development of A-14
    • A-21S - refined production version of A-21
    • A-21SJ - jet-powered version of A-21 using either a 0.16 or 0.20 kN (36 or 45 lbf) thrust engine, having a 10,000 m (33,000 ft) ceiling. A trailing edge flap-airbrake is unique to this model. Marketed in America by AVIA America Corporation.[2]

Specifications (A-21S)

Data from [3]

General characteristics

  • Crew: one, pilot
  • Capacity: one passenger
  • Length: 7.84 m (21 ft 9 in)
  • Wingspan: 20.38 m (66 ft 10 in)
  • Height: 1.61 m (5 ft 3 in)
  • Wing area: 16.2 m2 (174 sq ft)
  • Aspect ratio: 25.6
  • Empty weight: 436 kg (961 lb)
  • Gross weight: 644 kg (1,420 lb)

Performance

  • Maximum speed: 255 km/h (158 mph, 137 kn)
  • Maximum glide ratio: 43:1
  • Rate of sink: 0.60 m/s (118 ft/min)

References

  1. ^ "Caproni A-10 / A-12 / A-14 / A-20". all-aero.com. Retrieved 2022-05-16.
  2. ^ Air Progress: 20. October 1971. {{cite journal}}: Missing or empty |title= (help)
  3. ^ Coates, Andrew (1978). Jane's World Sailplanes and Motor Gliders. London: MacDonald and Jane's. p. 107.

Further reading

External links