Artistic illustration LL PSV © Konstantinos Panitsidis
Technical specifications Photos Video
Experimental helicopter based on the Mi-24K - prospective high speed helicopter.
Single-seat streamlined cockpit, unarmed, fitted with experimental main rotors for research into high-speed flight.
The first test flight of the helicopter Mi-PSV held on December 29, 2015.
PSV – Demonstrator: Prospective high speed helicopter
The innovation introduced in helicopter to the impeller which has blades with curved finish, new generation entirely made of synthetic materials developed by Mil.
The lack of wing
Using a new generation of blades allow: helicopter Mi-28NM
- of increasing the speed by 10%
- of increase the cruise speed by 13%
Using a new generation of blades allow: helicopter Mi-35M
- of increasing the speed by 13%
- of increase the cruise speed by 30%
PSV demonstrator is an experimental helicopter, based at the helicopter Mi-24K
TECHNICAL SPECIFICATIONS
DESIGNER
|
OKB Mil
|
TYPE
|
Prospective high speed helicopter (PSV) |
CREW
|
1
|
POWER-PLANT
|
Two engine VK-2500-01
|
Power, h.p.
|
2 x 2.400
|
DIMENSIONS
|
|
Length, m
|
-
|
Main rotor diameter, m
|
-
|
Tail rotor diameter, m
|
3,91
|
Wing span, m
|
6,66
|
Height, m
|
-
|
WEIGHT
|
|
Empty, kg
|
-
|
Normal take-off, kg
|
-
|
Maximum take-off, kg
|
11.500
|
PERFORMANCE
|
|
Maximum speed, km/h
|
up to 400
|
Cruising speed, km/h
|
340-360
|
Ferry range, km
|
-
|
Combat range, km
|
-
|
Service ceiling, m
|
6.200
|
Static ceiling, m
|
3.800
|
Payload, kg
|
-
|
or with on hook
|
-
|
ARMAMENT | - |