АВИКОН: АК-21
Avicon: AC-21

General data

Producer info

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Names and dates
Market original model designation
АК-21
Market model designation (english translation or spelling)
AC-21
Date of prototype completion
1995
Country of manufacture
Moldova
People involved
Alexander Satarov {Александр Сатаров}Chief design engineer
Config info
Rotorcraft typeAutogyro
Weights
Maximum Takeoff Weight (MTOW)
340
kg
Cabin and cockpit
Maximum number of people onboard
1
Powerplant
Engine model
Rotax 912
Number of engines
1
Total maximum power
80
HP
Performance
Maximum horizontal flight speed (Vh)
130
km/h
Cruise speed (Vc)
100
km/h
Minimum speed
35
km/h
Take-off distance
10
m
(...)
0
m
Landing speed
20
km/h
Landing distance
10
m
(...)
0
m
Best rate of climb
5
m/s
Maximum service ceiling
4000
m
Maximum range
270
km
0.0967