Ai-10 "Ikar" -
ultralight multipurpose for
two person aircraft
The instruction
on assembly, see
also
The
aircraft was designed to organize nets of aerial communication in a distance
to 1000 km., teaching pilot, and also
to decide such specific tasks.
|
|
Length |
6,21 m |
Stalling speed |
50 km/h |
| Height |
1,7 m |
Landing speed |
55 km/h |
| Wing span |
9,06 m |
Cruising speed |
160 (180) km/h |
| Wing area |
11,74 m2 |
Max speed |
246 km/h |
| Empty weight |
284 kg |
Vertical speed |
5 (6) m/s |
| Takeoff weight |
450 (510) kg |
Range |
920 (1000) km |
| Load factor |
+6/-3 |
Takeoff/landing run |
80/60 m |
| Engine ROTAX 912 (914) |
80 (100) hp |
Ceiling |
3500 (4000) m |
Ai-10 "Ikar" -
agriplane
|
|
Length |
6,21 m |
Stalling speed |
50 km/h |
| Height |
1,7 m |
Landing speed |
55 km/h |
| Wing span |
9,06 m |
Cruising speed |
150 (180) km/h |
| Wing area |
11,74 m2 |
Max speed |
200 km/h |
| Empty weight |
284 kg |
Vertical speed |
5 (6) m/s |
| Takeoff weight |
450 (510) kg |
Range |
920 (1000) km |
| Load factor |
+5/-2 |
Takeoff/landing run |
80/60 m |
| Engine ROTAX 912 (914) |
80 (100) hp |
Ceiling |
3500 (4000) m |
| Workload |
250 kg |
Productivity |
80-140 ga/h |
"Aist" - ultralight multipurpose for
two person aircraft
The
aircraft was designed to organize nets of aerial communication in a distance to 200
km., teaching pilot, and also to decide such specific tasks.
|
|
Length |
6,21 m |
Stalling speed |
55 km/h |
| Height |
1,7 m |
Landing speed |
65 km/h |
| Wing span |
11 m |
Cruising speed |
80 km/h |
| Wing area |
14,2 m2 |
Max speed |
120 km/h |
| Empty weight |
210 kg |
Vertical speed |
4 m/s |
| Takeoff weight |
450 kg |
Range |
200 km |
| Load factor |
+4/-2 |
Takeoff/landing run |
60/70 m |
| Engine ROTAX 582 |
64 hp |
Ceiling |
3000 m |
Motorglider of balance
"Zhuravlik"
 |
Wing span |
9,6 m |
| Wing area |
14,4 m2 |
| Takeoff weight |
145 kg |
| Engine power |
20 h.p. |
| Max speed |
50 km/h |
| Landing speed |
25 km/h |
| Range |
80 km |
| Ceiling |
2000 m |
|
