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Ka-50 Black Shark (Hokum A) Russian Attack Helicopter

Kamov Ka-50 "Black Shark", Hokum A

Attack Helicopter
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Basic Information
Name
Ka-50 Black Shark (Hokum A) Russian Attack Helicopter
Designation
Kamov Ka-50 "Black Shark", Hokum A
Alternate Designation
Kamov Ka-50 "Black Shark", Hokum A
Equipment Type
Attack Helicopter
Manufacturer
Kamov
Date of Introduction
1995
Description

The Ka-50, also nicknamed the Chernaya Akula (Black Shark) was a Soviet attack helicopter. Its NATO reporting name was Hokum. The Ka-50 was planned as a rival to the Mi-28 in a competition to provide the Soviet armed forces with a new battlefield attack helicopter. Kamov opted for a single-crew layout to save weight for more armor, more powerful armament, and a greater number of advanced sensors. The first of three V-80 prototypes made its maiden flight on 17 June 1982. In October 1986 the Ka-50 was selected for production. With the collapse of the Soviet Union, Russia faced military budget cuts. Production of the original Ka-50 was stopped with only around 10 of these helicopters ever built. In 2000 a pair of production Ka-50 helicopters was used during the Second Chechen War, where these gunships were basically tested by the Russian military to evaluate the type. However the original Ka-50 never reached full operational capability. If the Ka-50 is to operate at night, it must be equipped with a Saturn night targeting pod. This pod takes up one of the underwing pylons. This Ka-50 never entered full rate production and subsequently never fielded beyond several prototypes delivered for operational testing. Only a handful of prototypes exist and have not yet been approved for additional production. It is assessed the KA-50 prototypes remain in limited service with the Russian Air Force.

Air & Air Defense Specifications
Crew 1
Engine Turboshaft (2200 hp)
Max Speed 350.0 km/h
Range 250.0 km
Endurance 3.00 hrs
Wingspan 7.30 m
Rotor Diameter 14.50 m
Variants
Kamov V-80 Prototype version for Ka-50.
Kamov Ka-50 Single-seat version.
Kamov Ka-50N Ka-50 with night attack capability.
Kamov Ka-50Sh Ka-50 with improved night attack capability.
Kamov Ka-50-2 "Erdogan" Version with a two-seat tandem cockpit.
Kamov Ka-52 "Alligator" Highly upgraded version with a two-seat side-by-side cockpit for the Russian Air Force.
Kamov Ka-52K "Katran" Naval version with folding blade and reinforced landing gear, wing shortened for basing on ships and the possibility of using Kh-35 anti-ship missile.
System
Alternative Designation Kamov Ka-50 "Black Shark", Hokum A
Type Single-seat attack helicopter
Manufacturer Kamov
In Service 1995-Present
Crew 1 ea
Blades, Main Rotor Each rotor has three blades with swept tips
Blades, Tail Rotor No tail rotor necessary in this configuration
Number of Engines 2 ea
Day/Night Capable The Ka-50N Night Shark was developed to overcome the challenges of operating at night that the ka-50 has.
All Weather Capable Yes
Takeoff or Landing Limitations INA
Number of Hard Points 4 (6 on Ka-52) under-wing hardpoints, plus 2 on wingtips for countermeasures or air-to-air missiles with a capacity of 2,000 kg
Digital Autopilot Yes
Maximum Pylons Capacity 2,300 kg
Landing Gear Two-wheel nose landing gear retracts to the rear under the cockpit
Note #1 The lack of a tail rotor enables the aircraft to perform flat turns within the entire flight speed range
Note #2 If the Ka-50 is to operate at night, it must be equipped with a Saturn night targeting pod. This pod takes up one of the underwing pylons
Dimensions
Length with Rotors 16 m
Rotor Diameter 14.50 m
Wingspan 7.30 m
Height 4.90 m
Weight, Empty 7,692 kg
Weight, Takeoff Normal 9,800 kg
Weight, Takeoff Maximum 10,800 kg
Disc Area 330.4 m sq
Automotive
Engine Name 2 x turboshaft Klimov TV3-117VMA
Engine Type Turboshaft
Engine Power 2,200 shaft hp each
Speed, Maximum Level 315 km/h
Speed, Maximum Dive 350 km/h
Speed, Cruise 270 km/h
Speed, Backwards 90 km/h
Speed, Sideways 70 km/h
Range, Combat Radius 250 km
Range, Normal Radius 460 km
Range, Ferry 1,160 km
Climb Rate 600 m/min
Ceiling Hover 4,000 m
Ceiling Service 5,500 m
Load Factor 3.5 g (max vertical)
Endurance 3 Hours
Communications
Radio INA
Chin Mounted Gun
System
Name Shipunov 2A42,
Type 30mm Autocannon
Manufacturer Tulamashzavod
In Service 1980-Present
Length 3.027 m
Barrel Length 2,416 mm
Barrels 1 ea
Action Gas-operated
Rate of Fire, Low 200 to 300 rds/min
Rate of Fire, High 550-800 rds/min (high)
Effective Firing Range (AP-t) 2,000 m
Maximum Firing Range (HEI) 4,000 m
Feed System Twin Feed
Ammunition
Name 3UOF8
Type HEI
Caliber 30 mm
Cartridge 30 × 165
Muzzle Velocity 960 m/s
Basic Load 2,000 ea
Armor Penetration INA
Projectile Weight 389 grams
Bursting Charge 49 grams
Note A high-explosive incendiary round with A-670M nose fuse.[10] The fuse produces a 0.15 millisecond delay on impact, and a self-destruct mechanism detonating the projectile after 7.5 to 14.5 seconds of flight (3900–5300 m distance from muzzle).
Wing Mounted Weapons
Note The Ka-50 can also be outfitted with the Kh-25MP (AS-12 Kegler) Missile and FAB 500 or tactical dispensers
Rocket System
Name S-8 Rocket
Type Rocket
Rocket Pod Type B series of rocket pods, carrying either seven or 20 rockets.
Number of Rocket Pods 4 ea
Rocket Length 1.56 m
Rocket Diameter 80 mm
Launch Weight 11.5 kg
Warhead Type HEAT
Warhead Weight 3.6 kg
Basic Load 80 separate S-80 Rockets in four B-8 Series Rocket Pods ea
Maximum Effective Range 4 km
Minimum Effective Range 1.3 km
Speed 692 m/s
Armor Penetration 350 mm versus RHA
Fuze Type N-26A fuze
Motor BIK-2D motor powder
Missile System
Name R-60 Missile (AA-8 Aphid")
Type Short-range lightweight infrared homing air-to-air missile
In Service 1974-Present
Manufacturer Vympel
Length 2,090 mm
Diameter 120 mm
Wingspan 390 mm
Basic Load INA
Warhead Type 3 kg
Detonation mechanism Proximity
Engine Solid-fuel rocket engine
Operational Range 8 km
Flight Altitude 20,000 m
Speed Mach 2.7
Guidance System Infrared Homing
Note The Ka-50 can also carry the R-73 (AA-11 Archer) Missile
Anti-Tank Guided Missile System
Name 9K121 Vikhr (AT-16 Scallion)
Type Laser-Guided ATGM Missile
In Service 1985-Present
Length 2.80 m
Diameter 130 mm
Wingspan 380 mm
Missile Weight 45 kg
Warhead Type Tandem HEAT charge
Warhead Weight 8-12 kg
Armor Penetration (ERA) 1,000 mm
Basic Load 12 ea
Detonation Mechanism Proximity and Impact
Engine Solid-fuel rocket
Propellant Sold Fuel
Operational Range 10-12 km
Speed 600 m/s
Guidance System Laser beam riding
Note The Ka-50 can also carry 9M120 Ataka (Spiral-2) ATGMs.
Fire Control
Fire Control System Type INA
Fire Control Radar Millimeter wave radar
Digital or Analog Cockpit Digital
Direct Fire Control Yes
Laser Designator Yes
Laser Rangefinder Yes
Night Vision Electro-optical sight; takes one pylon slot
Position Location System Yes
IFF Yes, Slap Shot System
Heads Up Display (HUD) Yes
Helmet-Mounted Display Yes
Data Link Yes, with ground units
Protection
Armor Protection against 12.7-mm armor-piercing bullets and 23-mm projectile fragments
Cockpit Glass INA
Stealth Properties No
Heat Signature Reduction Yes, Exhaust infrared (IR) suppressors
Add on Armor INA
NBC Protection Yes
EW Counter System Yes
Counter Measures (Chaff/Flares) Yes, launchers in wingtip pods
Ejection System K-37-800 rocket-assisted
Automatic Fire Suppression System Yes
Note #1 Extensive provision of steel armor adds 770 lb (350 kg) to aircraft weight.
Note #2 Armored, self-sealing composite fuel cells are buried in the fuselage.
Details
Country of Origin Russia
Category Rotary Wing Aircraft
Air > Rotary Wing Aircraft
Filter Label
K
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
16 m
Width
7.3 m
Height
4.9 m
Weight
9800 kg
Operators (1)
Russia
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