Manufacturer | Ikarus |
Model | 453(P-453-MW) |
Modification | 453 |
Country | Yugoslavia |
Years | 19 |
Type | Experimental aircraft |
Main rotor diameter | - |
Tail rotor diameter | - |
Wingspan | 7.50 m |
Length | 5.85 m |
Height | 2.01 m |
Wing area | - |
Zero fuel weight | - |
Empty weight | - |
Maximum takeoff weight | 1720 kg |
Normal takeoff weight | - |
Flight duration | - |
Engine | 1 ТРД Turbomeca Marbord II |
Power | - |
Thrust | 1 x 3.91 kN |
Maximum speed | - |
Cruising speed | - |
Rate of climb | - |
Practical range | - |
Service ceiling | - |
Hovering ceiling | - |
Crew | 1 |