Basic Information
| Category | Helicopter | Type | Attack |
| Year Commissioned | 2018 | Year Decommissioned | 0 |
| Agility | 2 | Damage Points (DP) | 5 |
| Empty Weight | 7700 kg | Max Weight | 10800 kg |
| Runway Information | 0m (VTOL) TOD/LAD | Physical Size | Medium Aircraft (12.1-18m) |
| Cost | 0 | Hypothetical | No |
| Payload Weight | 2000 kg | Crew | 2 people |
Aircraft Capabilities
Nap-of-the-Earth (NOE)
Night Navigation/Attack (Incl. Bomb, Rocket Delivery)
Bombsight - Advanced Computing
IRSS - Peak Temp Reduction (Cool-Air Mix)
Sensor Parameters
| Model | Purpose | Range | Scan Interval | Generation |
| FH01 Arbalet 52 | Radar, FCR, Air-to-Air & Air-to-Surface, Short-Range | 0.10 - 20.00 nm | 2 sec | Early 2000s |
| OES-52 [IR/TV/Laser Designator] | Sensor Turret | 0.00 - 0.00 nm | 0 sec | Not Applicable (N/A) |
| L-370 Vitebsk | Sensor Group | 0.00 - 0.00 nm | 0 sec | Not Applicable (N/A) |
Sensor Coverage Diagram
| Model | Detection Angle | Omnidirectional |
| FH01 Arbalet 52 | SB1, SB2, SMF1, PB1, PB2, PMF2 | 否 |
| OES-52 [IR/TV/Laser Designator] | SB1, SB2, SMF1, SMF2, SMA1, SMA2, SS1, SS2, PB1, PB2, PMF1, PMF2, PMA1, PMA2, PS1, PS2 | 是 |
| L-370 Vitebsk | SB1, SB2, SMF1, SMF2, SMA1, SMA2, SS1, SS2, PB1, PB2, PMF1, PMF2, PMA1, PMA2, PS1, PS2 | 是 |
Weapon Loadouts Click to Expand Beta
| Loadout Type | Role | Ready Time | Combat Radius | ||||
|---|---|---|---|---|---|---|---|
| (Ferry) | Ferry | 30 min | 520 nm | ||||
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| (Reserve [Available]) | Reserve | 180 min | 0 nm | ||||
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| (Maintenance [Unavailable]) | Unavailable | 0 min | 0 nm | ||||
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| AT-9 Spiral-2 [9M120 Ataka-V], S-8KO 80mm Rockets | BAI/CAS | 360 min | 220 nm | ||||
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| S-13B 122mm Rockets | BAI/CAS | 360 min | 220 nm | ||||
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| S-5K 57mm Rockets | BAI/CAS | 360 min | 220 nm | ||||
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| S-8KO 80mm Rockets | BAI/CAS | 360 min | 220 nm | ||||
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| AT-16 Scallion [9A1472 Vikhr-1], S-8KO 80mm Rockets | BAI/CAS | 360 min | 220 nm | ||||
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| AT-16 Scallion [9A1472 Vikhr-1], S-8KO 80mm Rockets, Long-Range | BAI/CAS | 360 min | 400 nm | ||||
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| AT-16 Scallion [9A1472 Vikhr-1], S-8KO 80mm Rockets, Heavy Igla-V, Long-Range | BAI/CAS | 360 min | 400 nm | ||||
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Signatures
| Type | Front | Side | Rear |
|---|---|---|---|
| Visual Detection Range | 1.99 nm | 5.93 nm | 1.99 nm |
| Visual Classification Range | 1.17 nm | 3.37 nm | 1.83 nm |
| Infrared Detection Range | 1.99 nm | 6.97 nm | 10.09 nm |
| Infrared Classification Range | 1.17 nm | 3.37 nm | 1.17 nm |
| Radar, A-D Band (30-2000 MHz) | 1.8 dBsm (1.51 m²) | 4.3 dBsm (2.69 m²) | 1.8 dBsm (1.51 m²) |
| Radar, E-M Band (2-100 GHz) | 1.8 dBsm (1.51 m²) | 4.3 dBsm (2.69 m²) | 1.8 dBsm (1.51 m²) |
Default Configuration
| Model | Comments |
|---|---|
| 30mm 2A42 [240 rnds] | Helicopter, Ka-52 |
| UV-26 x 4 [512 Cartridges] | Ka-50, Chaff & Flare Dispenser |
Datalink
| Type | Model | Range | Channels |
|---|---|---|---|
| Radio | UHF/VHF Radio [Unsecure] | 100 nm | 0 |
| Radio | VHF Radio [Unsecure] | 100 nm | 0 |
| Radio | AT-2/6/8/9 Guidance Unit | 10 nm | 1 |
Engines
| Model | Type | Engine Count | Military Thrust | Afterburner Thrust | Military Fuel Rate (SFC) | Afterburner Fuel Rate (SFC) | Hypothetical | Comments |
|---|---|---|---|---|---|---|---|---|
| 2x VK-2500 | Helo Turboshaft | 2 | 2400 | - | 0.21 | - | No | - |
Fuel
| Fuel Type | Fuel Capacity |
|---|---|
| Aviation Fuel | 1200 |