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. Template:ISBN
General characteristics
- Crew: 1
- Capacity: 1 passengerTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convert
- Aspect ratio: 19:1
- Airfoil: NACA 63618 (root); NACA 63615 (tip)Template:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/engTemplate:Aircraft specs/engTemplate:Aircraft specs/engTemplate:Aircraft specs/lengthTemplate:Aircraft specs/convertTemplate:Aircraft specs/length
PerformanceTemplate:Aircraft specs/speedTemplate:Aircraft specs/speedTemplate:Aircraft specs/speedTemplate:Aircraft specs/speedTemplate:Aircraft specs/speedTemplate:Aircraft specs/rangeTemplate:Aircraft specs/rangeTemplate:Aircraft specs/rangeTemplate:Aircraft specs/convert
- Maximum glide ratio: 32Template:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertScript error: No such module "Check for unknown parameters".
See also
Related development
Aircraft of comparable role, configuration, and era
Related lists
References
Notes
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References
- Coates, Andrew. “Jane's World Sailplanes & Motor Gliders new edition”. London, Jane's. 1980. Template:ISBN
External links
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- History of the M-200 Retrieved 8 July, 2020