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Ka-25BSh 'Hormone-A' |
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Entered service |
1967 |
|
Crew |
? |
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Dimensions and weight |
|
Length |
9.75 m |
|
Rotor diameter |
15.74
m |
|
Height |
5.37
m |
|
Weight (empty) |
4.76 t |
|
Weight (maximum take off) |
7.5 t |
|
Engines and performance |
|
Engines |
2 x OMKB 'Mars' GTD-3F turboshafts |
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Engine power |
2 x 898 hp |
|
Maximum speed |
209 km/h |
|
Service ceiling |
3.3 km |
|
Range |
400 km |
|
Armament |
|
Torpedoes |
provision for torpedoes |
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Other |
conventional or nuclear depth charges |
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Designed to
meet a 1957 Soviet navy requirement for a new shipborne ASW
helicopter, the first member of the Ka-20/25 family was the Ka-20
Harp, which initially flew during 1960. The production Ka-25BSh
Hormone-A was of near identical size and appearance, but was fitted
with operational equipment and uprated GTD-3F turboshaft engines
(from 1973 these were replaced by GTD-3BMs). It entered service in
1967.
Although the
lower part of the fuselage is sealed and watertight, the Ka-25 is
not intended for amphibious operations, and flotation bags are often
fitted to the undercarriage for use in the event of a emergency
landing on the water. The cabin is adequate for the job, but is not
tall enough to allow the crew to sand upright. Progressive additions
of new equipment have made the interior more cluttered.
Primary
sensors for the anti-submarine warfare mission are the I/J-band radar (ASCC/NATO Big
Bulge), OKA-2 dipping sonar, a downward-looking Tie Rod
electro-optical sensor in the tailboom and a magnetic anomaly
detection (MAD) sensor, either in a
recess in the rear part of the cabin or in a fairing sometimes
fitted below the central of the three tailfins. A box-like sonobuoy
launcher can also be scabbed on to the starboard side of the rear
fuselage. Dye-markers or smoke floats can also be carried
externally. Comprehensive avionics, defensive and navigation systems
are also fitted as standard.
Armament is
not normally carried, although the helicopter can be fitted with a
long coffin-like weapons bay which runs along the belly from the
radome back to the tailboom, and small bombs or depth charges can be
carried on tiny pylons just aft of the nosewheels. The underfuselage
bay can carry a variety of weapons, including nuclear depth charges.
When wire-guided torpedoes are carried, a wire reel is mounted on
the port side of the forward fuselage.
It has been
estimated that some 260 of the 450 or so Ka-25s produced were
Hormone-As, but only a handful remains in Russian and Ukrainian
service, mostly fulfiling secondary roles. Small numbers of
Ka-25BShs were exported to India, Syria, Vietnam and former
Yugoslavia, and most of these aircraft still remain in use.
The second
Ka-25 variant identified in the West was given the NATO reporting
name Hormone-B, and is designated Ka-25K. This variant is externally
identifiable by its bulbous (instead of flat-bottomed) undernose
radome and small datalink radome under the rear fuselage. Ka-25K was
used for acquiring targets and providing mid-course missile
guidance, for ship- and submarine-launched missiles. On the
Hormone-B only, the four undercarriage units are retractable and can
be lifted out of the scanning pattern of the radar.
The final
version of the military Ka-25 is the Ka-25PS Hormone-C. A dedicated
search and rescue (SAR) and transport helicopter, the Ka-25PS can carry a practical load
of freight or up to 12 passengers, making it a useful ship-to-ship
or ship-to-shore transport and vertrep platform. A quadruple Yagi
antenna (Home Guard) fitted to many aircraft is reportedly used for
homing on to the personal locator beacons carried by aircrew. Most
Ka-25PSs also have searchlight, and a 300-kg capacity
rescue winch. Ka-25PS has largely been replaced by
Ka-27.
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Video of the Ka-25 Hormone utility
helicopter |
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