Prospective high speed helicopter (PSV) © Konstantinos Panitsidis

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 © Konstantinos Panitsidis 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.

 

PSV The lack of wing © Konstantinos Panitsidis  
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% 

 

Το PSV PSV demonstrator is an experimental helicopter, based at the  helicopter Mi-24K © Konstantinos Panitsidis
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 -