Мi-28NE "Night Hunter"
 
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