Technical specifications
|
|
Type 1
|
Type 2
|
| Power unit, pcs
|
2-4 electric motors
|
2 ICE
|
| Take-off mass without gas, (on take-off with helium has a “null” floatability), kg
|
23–30
|
75
|
| Envelope length*, m
|
8,7
|
12,7
|
| Envelope diameter*, m
|
2,25–2,63
|
3,19
|
| Speed, km/h
|
0–40
|
0–40
|
| Altitude, m
|
up to 500
|
up to 500
|
| Flight range (radio line of sight and normal weather), km
|
up to 50
|
up to 50
|
| Endurance (at zero wind and air speed up to 3.7 m/s), h
|
up to 4
|
up to 6
|
| Payload capability, kg
|
up to 1,5
|
5,0
|
*EM UAS has possibility of large length and diameter implementation
