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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