9. On base of "EKIP-2" may be manufactured two-plases apparat with parameters

Characteristic Parameter Value
1. Maximum take-off weight
1000 kg
2. Cruising speed
250 km/h
3. Maximum speed
300 km/h
4. Flight altitude, m
20 ~ 5000 m
5. Maximum flight duration
3 hours
6. Length
3,6 m
7. Wingspan
6,482 m
8. Height
1,423 m
9. Take-off speed
100 km/h
10. Landing speed
95 km/h
11. Take-off roll ground/water
180/230 m
12. Landing roll ground/water
100/120 m
13. Specific pressure on ground (water)
182 kg/m2
14. Fuel tank capacity
400 liters


 

1.
Description of Flying Vehicles "EKIP"
2.
Basic Technical Concepts of the "EKIP" Project
3.
Patents
4.
Basic Advantages of Flying Vehicles "EKIP" Compared to Traditional Airplanes
5.
CONDITION OF WORKS ON ZAO "AC "EKIP" PROJECT
6.
GOVERNMENTAL SUPPORT OF "EKIP" PROJECT
7.
AUTOMATIC CONTROL PATROL AND RECONNAISSANCE FLYING VEHICLES "EKIP-AULA L2-3"
8.
AUTOMATIC CONTROL PATROL AND RECONNAISSANCE FLYING VEHICLES "EKIP-2"
9.
On base of "EKIP-2" may be manufactured two-plases apparat with parameters
10.
FLIGHT AND TECHNICAL CHARACTERISTICS OF "EKIP" FLYING VEHICLES
11.
Cost of Design and Organization of Production Of Flying Vehicles 'EKIP" ($ Million)
12.
Schedule of Implementation of Program "Flying Vehicles "EKIP". Volume of Production
13.
Schedule of Implementation of Project "EKIP L2-3". Costs, Payback $M
14.
Schedule of Implementation of Project "EKIP L3-1". Costs, Payback $M
15.
Schedule of Implementation of Project "EKIP L3-2". Costs, Payback $M

 

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