Basic Information
| Category | Helicopter | Type | Transport |
| Year Commissioned | 2019 | Year Decommissioned | 0 |
| Agility | 1 | Damage Points (DP) | 5 |
| Empty Weight | 5270 kg | Max Weight | 11200 kg |
| Runway Information | 0m (VTOL) TOD/LAD | Physical Size | Medium Aircraft (12.1-18m) |
| Cost | 0 | Hypothetical | No |
| Payload Weight | 0 kg | Crew | 3 people |
Aircraft Capabilities
Nap-of-the-Earth (NOE)
Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles)
IRSS - Shielded Exhaust (Jet Deviation)
IRSS - Peak Temp Reduction (Cool-Air Mix)
Sensor Parameters
| Model | Purpose | Range | Scan Interval | Generation |
| AN/APS-143 | Radar, Surface Search, Long-Range | 0.50 - 200.00 nm | 5 sec | Late 1990s |
| AN/AAQ-21/22 Star Safire III Multi-Sensor Turret [FLIR/CCD/Laser Designator] | Sensor Turret | 0.00 - 0.00 nm | 0 sec | None |
| RWS-300 [IDAS-3] | RWR, Radar Warning Receiver | 0.00 - 120.00 nm | 5 sec | Late 2000s |
| MAW-300 [IDAS-3] | MAWS, Missile Approach Warning System | 0.00 - 5.00 nm | 60 sec | Early 2010s |
| LWS-310 [IDAS-3] | LWR, Laser Warning Receiver | 0.00 - 6.00 nm | 5 sec | Early 2000s |
Sensor Coverage Diagram
| Model | Detection Angle | Omnidirectional |
| AN/APS-143 | SB1, SB2, SMF1, SMF2, SMA1, PB1, PB2, PMF1, PMF2, PMA2 | 否 |
| AN/AAQ-21/22 Star Safire III Multi-Sensor Turret [FLIR/CCD/Laser Designator] | SB1, SB2, SMF1, SMF2, SMA1, SMA2, SS1, SS2, PB1, PB2, PMF1, PMF2, PMA1, PMA2, PS1, PS2 | 是 |
| RWS-300 [IDAS-3] | SB1, SB2, SMF1, SMF2, SMA1, SMA2, SS1, SS2, PB1, PB2, PMF1, PMF2, PMA1, PMA2, PS1, PS2 | 是 |
| MAW-300 [IDAS-3] | SB1, SB2, SMF1, SMF2, SMA1, SMA2, SS1, SS2, PB1, PB2, PMF1, PMF2, PMA1, PMA2, PS1, PS2 | 是 |
| LWS-310 [IDAS-3] | 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 | 475 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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| Search And Rescue (SAR) | Search And Rescue (SAR) | 60 min | 230 nm | |
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| Cargo, 5 tons, Slung Load | Cargo Transport | 120 min | 100 nm | |
| Cargo, 3 tons | Cargo Transport | 120 min | 330 nm | |
| Troops, 20x | Troop Transport | 120 min | 350 nm | |
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Signatures
| Type | Front | Side | Rear |
|---|---|---|---|
| Visual Detection Range | 2.11 nm | 6.06 nm | 2.11 nm |
| Visual Classification Range | 1.23 nm | 3.43 nm | 1.93 nm |
| Infrared Detection Range | 2.11 nm | 7.07 nm | 10.3 nm |
| Infrared Classification Range | 1.23 nm | 3.43 nm | 1.23 nm |
| Radar, A-D Band (30-2000 MHz) | 2.5 dBsm (1.78 m²) | 4.9 dBsm (3.09 m²) | 2.5 dBsm (1.78 m²) |
| Radar, E-M Band (2-100 GHz) | 2.5 dBsm (1.78 m²) | 4.9 dBsm (3.09 m²) | 2.5 dBsm (1.78 m²) |
Default Configuration
| Model | Comments |
|---|---|
| 7.62mm MG [400 rnds] | Helicopter |
| 7.62mm MG [400 rnds] | Helicopter |
| BOP-L | Dual Spectral, Chaff & Flare Dispenser |
| BOP-L | Dual Spectral, Chaff & Flare Dispenser |
Datalink
| Type | Model | Range | Channels |
|---|---|---|---|
| Radio | UHF/VHF Radio [Secure] | 100 nm | 0 |
Engines
| Model | Type | Engine Count | Military Thrust | Afterburner Thrust | Military Fuel Rate (SFC) | Afterburner Fuel Rate (SFC) | Hypothetical | Comments |
|---|---|---|---|---|---|---|---|---|
| 2x Makila 2A1 | Helo Turboshaft | 1 | 2382 | - | 0.5 | - | No | - |
Fuel
| Fuel Type | Fuel Capacity |
|---|---|
| Aviation Fuel | 2030 |