Мi-28NE
Performance | |
|---|---|
|
Normal take-off weight
|
10,900 kg |
|
Speed (ISA, H= 0)
|
220 km/h |
|
Maximum
|
300 km/h |
|
Cruise
|
270 km/h
|
|
Hover ceiling (ISA, OGE)
| 3,600 m |
|
Operational ceiling (ISA, OGE)
| 5,600 m |
|
Engine type
| VK-2500 |
|
Take-off power
| 2×2,200 h. p. |
Primary weapons: | |
|
air-to-ground missile armament suites «Ataka-B» and «IGLA»
| |
|
air-to-air missile armament suites «Strelets»
| |
|
movable gun mount with gun of cal. 30 mm
| |
|
НАР Б-8В20А rocket pods with S-8 and НАР Б-13Л1 rocket
| |
|
S-13 rocket pods of cal. 80 mm и 130 mm
| |
|
airborne radar over the rotor hub assembly
| |
|
round-the-clock target sight system ОПС-28 М
| |
Possibilities: | |
|
round-the-clock operation in adverse and friendly weather conditions
| |
|
killing of enemy armored targets using guided weapons
|
. |
|
manual and automatic nap-of-the-earth flight
|
. |
|
stand-alone solo stationing
|
. |
|
reliable armoring
|
. |
Defense suite: |
|
spacing of engines
| |
|
insulation of engines by airframe elements
| |
|
composite materials used for fabrication of main rotor and tail rotor blades
| |
|
redundancy of fuel, hydraulic and pneumatic mains
| |
|
shielding of vital units by units of secondary importance
| |
|
filling of airframe spaces by foam material
| |
|
armoring of cockpit and vital units
| |
|
fire protection of power plant, hydraulic systems, other fire hazardous units and compartments
| |
|
explosion protection of fuel tanks (by foam polyurethane)
| |
|
protection of fuel tanks from fuel leakage from holes (self-sealing,
| |
|
use of diaphragms
| |
|
application of nonflammable fluids
|
Crew survivability is provided by: |
|
installation of shock absorbing crew seats with parachute escape system
| |
|
shock absorbing landing gear
| |
|
installation of emergency jettisoning system for portside and starboard cockpit doors and wing panels
| |
|
installation of inflatable rubber bags for avoidance of collision with landing gear at emergency abandoning
| |
