- Source: CVT M-200
The CVT M-200 was a two-seat glider that was designed in Italy and built in Italy and France from 1963.
Development
Designed by Alberto and Piero Morelli, the M-200 was built by the Turin Gliding Centre (Centro di Volo a Vela – Turin) under contract with the Aero Club of Italy (Aero-club d'Italia). The M-200 is a two-seat glider with dual controls with generally similar layout to the single seat M-100 but with greater dimensions. Conventional wooden-frame structure and plywood skinning were used for the fuselage with a single-spar wing covered in plywood and fabric. Accommodation for two is provided in the staggered seat cockpit covered by a sideways hinging canopy. With relatively high performance for its day, the M-200 proved to be easy to fly both for early solo pilots and for advanced aerobatics.
The M-200 was also built in France by CARMAM as the M-200 Foehn.
Specifications (M-200)
Data from Coates, Andrew. “Jane's World Sailplanes & Motor Gliders new edition”. London, Jane's. 1980. ISBN 0-7106-0017-8General characteristics
Crew: 1
Capacity: 1 passenger
Length: 7.6 m (24 ft 11.25 in)
Wingspan: 18.15 m (59 ft 6.5 in)
Wing area: 17.5 m2 (188.4 sq ft)
Aspect ratio: 19:1
Airfoil: NACA 63618 (root); NACA 63615 (tip)
Empty weight: 345 kg (761 lb)
Gross weight: 570 kg (1,257 lb)
Performance
Maximum speed: 225 km/h (140 mph, 120 kn)
Maximum glide ratio: 32
Rate of sink: 0.70 m/s (138 ft/min)
See also
Related development
CVT M-100 single-seat glider
CVT M-300 single-seat glider
Aircraft of comparable role, configuration, and era
LET L-13 Blanik
Schleicher ASK 13
Related lists
List of aircraft
List of gliders
References
= Notes
== References
=Coates, Andrew. “Jane's World Sailplanes & Motor Gliders new edition”. London, Jane's. 1980. ISBN 0-7106-0017-8
External links
History of the M-200 Retrieved 8 July, 2020
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