Basic Information
| Category | Helicopter | Type | Attack |
| Year Commissioned | 2016 | Year Decommissioned | 0 |
| Agility | 2 | Damage Points (DP) | 5 |
| Empty Weight | 8250 kg | Max Weight | 12000 kg |
| Runway Information | 0m (VTOL) TOD/LAD | Physical Size | Medium Aircraft (12.1-18m) |
| Cost | 0 | Hypothetical | No |
| Payload Weight | 1480 kg | Crew | 2 people |
Aircraft Capabilities
Nap-of-the-Earth (NOE)
Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles)
Bombsight - Ballistic Computing
IRSS - Peak Temp Reduction (Cool-Air Mix)
Sensor Parameters
| Model | Purpose | Range | Scan Interval | Generation |
| APS-17 WPM-W [IR/EO] | Sensor Turret | 0.00 - 0.00 nm | 0 sec | Not Applicable (N/A) |
| FPM-1KB Laser Designator | Laser Target Designator & Ranger (LTD/R) | 0.00 - 10.00 nm | 0 sec | Not Applicable (N/A) |
| Generic Night Vision Goggles | LLTV, Night Vision Goggles (NVG) | 0.00 - 15.00 nm | 10 sec | LLTV, 3rd Generation (2000s/2010s) |
| SPO-10 Sirena-3M | RWR, Radar Warning Receiver | 0.00 - 120.00 nm | 5 sec | Early 1970s |
| KT-01 IRCM | IRCM | 0.00 - 0.00 nm | 0 sec | Early 2010s |
Sensor Coverage Diagram
| Model | Detection Angle | Omnidirectional |
| APS-17 WPM-W [IR/EO] | SB1, SB2, SMF1, SMF2, PB1, PB2, PMF1, PMF2 | 否 |
| FPM-1KB Laser Designator | SB1, SB2, SMF1, SMF2, PB1, PB2, PMF1, PMF2 | 否 |
| Generic Night Vision Goggles | SB1, SB2, SMF1, SMF2, SMA1, PB1, PB2, PMF1, PMF2, PMA2 | 否 |
| SPO-10 Sirena-3M | SB1, SB2, SMF1, SMF2, SMA1, SMA2, SS1, SS2, PB1, PB2, PMF1, PMF2, PMA1, PMA2, PS1, PS2 | 是 |
| KT-01 IRCM | 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 | 540 nm | |||
| (Reserve [Available]) | Reserve | 180 min | 0 nm | |||
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| (Maintenance [Unavailable]) | Unavailable | 0 min | 0 nm | |||
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| AT-6 Spiral | BAI/CAS | 360 min | 150 nm | |||
| Troops, 8x, AT-6 Spiral | BAI/CAS | 360 min | 120 nm | |||
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| S-8 Rockets | BAI/CAS | 360 min | 150 nm | |||
| Barrier-V ATGM | BAI/CAS | 360 min | 150 nm | |||
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| Stugna-P [RK-2S] ATGM | BAI/CAS | 360 min | 150 nm | |||
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Signatures
| Type | Front | Side | Rear |
|---|---|---|---|
| Visual Detection Range | 2.01 nm | 6.19 nm | 2.01 nm |
| Visual Classification Range | 1.18 nm | 3.49 nm | 1.84 nm |
| Infrared Detection Range | 2.01 nm | 7.16 nm | 10.12 nm |
| Infrared Classification Range | 1.18 nm | 3.49 nm | 1.18 nm |
| Radar, A-D Band (30-2000 MHz) | 1.9 dBsm (1.55 m²) | 4.4 dBsm (2.75 m²) | 1.9 dBsm (1.55 m²) |
| Radar, E-M Band (2-100 GHz) | 1.9 dBsm (1.55 m²) | 4.4 dBsm (2.75 m²) | 1.9 dBsm (1.55 m²) |
Default Configuration
| Model | Comments |
|---|---|
| 30mm Gsh-30-2K [750 rnds] | Helicopter, Mi-24P, Fixed |
| ASO-3 x 2 [192 Cartridges] | Mi-8MT, Mi-24 Flare Dispenser |
Datalink
| Type | Model | Range | Channels |
|---|---|---|---|
| Radio | UHF/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 TV3-117VMA-SBM1V-02 | Helo Turboshaft | 2 | 2500 | - | 0.23 | - | No | - |
Fuel
| Fuel Type | Fuel Capacity |
|---|---|
| Aviation Fuel | 1500 |