|
|
10. FLIGHT AND TECHNICAL CHARACTERISTICS OF "EKIP" FLYING
VEHICLES
|
Characteristics
|
Type
of "EKIP Flying Vehicles
|
|
L2-3
|
L3-1
|
L3-2
|
| 1.
Full takeoff weight, tons |
12
|
45
|
360
|
| 2.
Commercial load, tons/pass |
4.0/40
|
16/160
|
120/1200
|
| 3.
Flight speed, km/h |
610
|
610
|
610
|
| 4.
Flight altitude, km |
11.5
|
11.5
|
11.5
|
| 5.
Range, km |
2500
|
4000
|
6000
|
| 6.
Fuel weight, tons |
2.7
|
14.0
|
127.2
|
| 7.
Length, m |
11.33
|
22
|
62
|
| 8.
Span, m |
18.64
|
36.2
|
102
|
| 9.
Height, m |
3.73
|
7.25
|
20.4
|
| 10.
Engines |
AL-342xPW
300
|
2xD4362xAL-34
|
6xD18T8xAL-34
|
| 11.
Thrust, tons |
2x2.35
|
2x9.0
|
6x25
|
| 12.
Thrust-to-weight ratio |
0.39
|
0.41
|
0.42
|
| 13.
Fuel consumption in cruising flight, g/pass/km |
15
|
15
|
15
|
| 14.
Air-cushion area, m2 |
45.6
|
170
|
1368
|
| 15.
Specific pressure on wing, kg/m2 |
<125
|
<125
|
<125
|
| 16.
Pressure on the runway, kg/m2 |
<265
|
<265
|
<265
|
| 17.
Runway length, m |
Up
to 450
|
Up
to 475
|
Up
to 600
|
| 18.
Runway type |
Ground,
water
|
Ground,
water
|
Ground,
water
|
|
