|
|
7.
AUTOMATIC CONTROL PATROL AND RECONNAISSANCE FLYING VEHICLES "EKIP-AULA
L2-3"
| Characteristic |
Parameter
Value |
| 1.
Full takeoff weight, kg |
280-350
|
| 2.
Payload, kg |
20-50
|
| 3.
Maximum flight speed, km/h |
300
|
| 4.
Cruiser flight speed, km/h |
180
|
| 5.
Flight altitude, m |
3000
|
| 6.
Maximum flying time, hours |
2
|
| 7.
Fuel weight, kg |
105
|
| 8.
Length, m |
2.03
|
| 9.
Span, m |
3.66
|
| 10.
Height, m |
0.71
|
| 11.
Engines |
1
(MD 120)
|
| 12.
Maximum thrust, kg |
120
|
| 13.
Maximum thrust of control engines, kg |
10
|
| 14.
Air-cushion area, m2 |
1.71
|
| 15.
Pressure on the runway, kg/m2 |
205
|
| 16.
Runway length, m |
Up
to 160
|
| 17.
Takeoff speed, km/h |
108
|
| 18.
Runway type |
Ground,
water
|
|
Stage
of Works
|
Cost
of million US dollars |
Period
of Performance, months |
| Design
and development |
0.7
|
4
|
| Manufacture
of 3 first vehicles |
2.0
|
8
|
| Ground
and flight tests |
1.8
|
9
|
| Preparation
of series production |
0.5
|
6
|
| Total: |
5.0
|
1.5
years with account for simultaneous works |
|
