Basic Information
| Category | Helicopter | Type | Unmanned Aerial Vehicle (UAV) |
| Year Commissioned | 2020 | Year Decommissioned | 0 |
| Agility | 1 | Damage Points (DP) | 3 |
| Empty Weight | 940 kg | Max Weight | 1430 kg |
| Runway Information | 0m (VTOL) TOD/LAD | Physical Size | UAS [NATO Class II] (150-600kg) |
| Cost | 0 | Hypothetical | No |
| Payload Weight | 272 kg | Crew | 0 people |
Aircraft Capabilities
Nap-of-the-Earth (NOE)
Night Navigation/Attack (Incl. Bomb, Rocket Delivery)
Sensor Parameters
| Model | Purpose | Range | Scan Interval | Generation |
| AN/AAQ-22D BRITE Star II [IR/EO/Laser] | Sensor Turret | 0.00 - 0.00 nm | 0 sec | None |
Sensor Coverage Diagram
| Model | Detection Angle | Omnidirectional |
| AN/AAQ-22D BRITE Star II [IR/EO/Laser] | 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 | 600 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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| Maritime Surveillance | Maritime Surveillance | 240 min | 300 nm |
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| HYDRA APKWS II 70mm Rockets | Strike, Land/Naval | 360 min | 280 nm |
Signatures
| Type | Front | Side | Rear |
|---|---|---|---|
| Visual Detection Range | 0.93 nm | 2.8 nm | 0.93 nm |
| Visual Classification Range | 0.58 nm | 1.67 nm | 0.81 nm |
| Infrared Detection Range | 1.04 nm | 5.04 nm | 8.7 nm |
| Infrared Classification Range | 0.68 nm | 1.97 nm | 0.68 nm |
| Radar, A-D Band (30-2000 MHz) | -9.1 dBsm (0.1230 m²) | -6.3 dBsm (0.2344 m²) | -9.1 dBsm (0.1230 m²) |
| Radar, E-M Band (2-100 GHz) | -12.1 dBsm (0.0617 m²) | -9.3 dBsm (0.1175 m²) | -12.1 dBsm (0.0617 m²) |
Default Configuration
| Model | Comments |
|---|
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 |
|---|---|---|---|---|---|---|---|---|
| 1x Rolls-Royce 250-C20W | Helo Turboshaft | 1 | 420 | - | 0.65 | - | No | - |
Fuel
| Fuel Type | Fuel Capacity |
|---|---|
| Aviation Fuel | 150 |