The Mil Mi-28 is developed to meet the demand of a Russian army requirement for a new close air support helicopter, main competitor is the Kamov Ka-50, until now no choice has been made between the two.
The five-blade main rotor is mounted above the body midsection, and short, wide, tapered, weapon-carrying wings are mounted to the rear of body midsection.
Developing Nation: | Russia. |
Task: | Two seat attack helicopter. |
First Flight: | November 10, 1982. |
First Delivery: | no production frames ordered. |
Crew: |
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Main rotor Span: | 17.20 m. |
Length: | 17.01 m (without rotors). |
Height: | 3.82 m to top of rotor head. |
Engine (s): | Klimov TV3 turbo shafts driving a five blade main rotor and four blade tail rotor 2x (2.465 hp each). |
Weight: | 8.590 kg. |
Max.Take off weight: | 11.500 kg. |
Max. Speed: | 320 km/h. |
Max. Range: |
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Weapons: |
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