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Ka-25

Ka-25

ASW Helicopters
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Basic Information
Name
Ka-25
Designation
Ka-25
Alternate Designation
Hormone, Ka-24PS, Ka-25BSh, Ka-25BShZ, Ka-25PL, Ka-25PS, Ka-25T
Equipment Type
ASW Helicopters
Manufacturer
Kamov
Date of Introduction
1963
Description

The Kamov Ka-25, dubbed Hormone by NATO, was a twin-engine shipborne helicopter developed in the early 1960s for the Soviet Navy as a replacement for Mil Mi-4 helicopter. The Ka-25 features two three-bladed coaxial counter rotating main rotors which eliminates the need for a tail rotor and makes the aircraft more compact which is highly appreciated in naval operations. The aircraft is equipped with magnetic anomalies detector (MAD), search radar and an electro-optical surveillance sensor similar to modern FLIR (Forward Looking Infrared). The former Soviet Union built approximately 460 such aircraft between 1966 and 1975. The Ka-25 was replaced by the more capable Ka-27 helicopter beginning in the 1980s. The Soviet Union deployed many variants of the Ka-25 helicopter intended to meet specific missions such as search and rescue (Ka-24PS/Ka-25PS), target acquisition (Ka-25T) during anti-surface warfare (ASuW) operations, utility (Ka-25PL), and Anti-Submarine Warfare (ASW). The primary ASW variant was the Ka-27BSh and the Ka-25BShZ was intended for towing minesweeping gear. The Ka-25 in ASW configuration can be armed with torpedoes and depth charges carried externally or using an optional internal weapons bay. The Ka-25PS and Ka-24PS aircraft were stripped of all ASW equipment and are fitted with a searchlight and a rescue winch. They can also serve as troops transport.

Air & Air Defense Specifications
Max Speed 209.0 km/h
Range 400.0 km
Service Ceiling 3500 m
Overview (Deagel)
Group ASW Helicopters
Status Active
Also Known As Hormone, Ka-24PS, Ka-25BSh, Ka-25BShZ, Ka-25PL, Ka-25PS, Ka-25T
Origin Russia
Contractor Kamov
Initial Operational Capability (IOC) 1963
Total Production 460
Specifications (Deagel)
Main Rotor Blades 6
Number of Engines 2
Dimensions — Height 5.4 meter
Dimensions — Length 9.8 meter
Dimensions — Main Rotor Diameter 15.7 meter
Mass — Max Takeoff Weight 7,100 kilogram
Mass — Payload 600 kilogram
Performance — Ceiling 3,500 meter
Performance — Max Range 400 kilometer
Power — Max Power at TakeOff 1,800 shp
Speed — Cruise Speed 193 kph
Speed — Top Speed at High Altitude 209 kph
Details
Country of Origin Russia
Category Rotary Wing Aircraft
Air > Rotary Wing Aircraft
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
9.8 m
Width
Height
5.4 m
Weight
7100 kg
Operators (5)
Russia
India
Serbia
Syria
Vietnam
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