|
Kamov Ka-27PL 'Helix-A' |
|
Entered service |
1982 |
|
Crew |
3 men |
|
Dimensions and weight |
|
Length |
11.27 m |
|
Main rotor diameter |
15.9
m |
|
Height |
5.45
m |
|
Weight (empty) |
6.1 t |
|
Weight (maximum take off) |
12.6 t |
|
Engines and performance |
|
Engines |
2 x Klimov TV3-117V turboshaft engines |
|
Engine power |
2 x 2 190 hp |
|
Maximum speed |
250 km/h |
|
Cruising speed |
230 km/h |
|
Service ceiling |
5 km |
|
Range |
800 km |
|
Combat radius |
km |
|
Payload |
|
Maximum payload |
5 t |
|
Typical load |
? |
|
Armament |
|
Torpedoes |
4 x APR-2E homing torpedoes |
|
Bombs |
4 x groups of S3V guided anti-submarine bombs in
place of torpedoes |
|
Development
of the
Ka-27 family began in 1969. The Ka-27 retains Kamov's well-proven
contra-rotating co-axial rotor configuration, and has dimensions
similar to those of the
Ka-25.
With more
than double the power of the Ka-25
Hormone, the
Ka-27 is a considerably heavier helicopter with a larger fuselage,
but nevertheless offers
increased performance with much-improved avionics and more modern
flight-control system.
The first
production variant was the Ka-27PL Helix-A basic anti-submarine
warfare (ASW) version, which
entered service in 1982. The Ka-27PL's fuselage is sealed over its
lower portions for buoyancy, while extra floatation equipment can be
fitted in boxes on the lower part of the centre fuselage. Ka-27 is
extremely stable and easy to fly, and automatic height hold,
automatic transition to and from the hover and autohover are
possible in all weather conditions. Ka-27PL has all the usual ASW
and ESM equipment including dipping sonar and sonobuoys as well as
Osminog (octopus) search radar.
The main
search and rescue (SAR)
and planetguard Ka-27 variant is the radar-equipped Ka-27PS Helix-D.
This usually carries external fuel tanks and flotation gear, and has
a hydraulically-operated, 300-kg capacity rescue winch.
Ka-28
Helix-A is the export version of the Ka-27PL ordered by China,
India, Vietnam and Yugoslavia and with a revised avionics suite.
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