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Institute of Aviation ZEM-94 Mozeta
This stick-controlled all-enclosed topless winged prototype was designed to evaluate wing performance by measuring deflection of the trike unit in relation to its drag.
Empty weight: 170 kg
Wing span: 10.2 m
Wing area: 15 sq.m
Fuel capacity: 20-60 lt
Engine: Rotax 503, 52 hp
MAUW: 360 kg
Seats: 2
Max speed: 150 kph
Cruise speed: 120 kph
Minimum speed: 60 kph
Climb rate: 6 m/s
Fuel consumption: 10 lt/hr
Price (1998): 45 000 PLZ

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