Basic Information
| Category | Fixed Wing | Type | Unmanned Combat Aerial Vehicle (UCAV) |
| Year Commissioned | 2002 | Year Decommissioned | 0 |
| Agility | 1 | Damage Points (DP) | 3 |
| Empty Weight | 513 kg | Max Weight | 1020 kg |
| Runway Information | 250-450m (STOL) TOD/LAD | Physical Size | Small Aircraft (0-12m) |
| Cost | 0 | Hypothetical | No |
| Payload Weight | 0 kg | Crew | 0 people |
Aircraft Capabilities
Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles)
Sensor Parameters
| Model | Purpose | Range | Scan Interval | Generation |
| AN/AAS-52 MTS-A [EO/IR/Laser Designator] | Sensor Turret | 0.00 - 0.00 nm | 0 sec | None |
Sensor Coverage Diagram
| Model | Detection Angle | Omnidirectional |
| AN/AAS-52 MTS-A [EO/IR/Laser Designator] | 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 | 2160 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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| AGM-114K Hellfire II | Strike, Land/Naval | 720 min | 1000 nm |
| Recon [Internal IR] | Unarmed Recon | 180 min | 1080 nm |
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| A/A: AIM-92E Stinger ATAS | Air Superiority, WVR AAMs | 180 min | 1100 nm |
Signatures
| Type | Front | Side | Rear |
|---|---|---|---|
| Visual Detection Range | 2.13 nm | 2.82 nm | 2.13 nm |
| Visual Classification Range | 1.15 nm | 1.69 nm | 1.84 nm |
| Infrared Detection Range | 2.37 nm | 5.07 nm | 11.99 nm |
| Infrared Classification Range | 1.36 nm | 1.98 nm | 1.36 nm |
| Radar, A-D Band (30-2000 MHz) | 0.9 dBsm (1.23 m²) | 3.2 dBsm (2.09 m²) | 0.9 dBsm (1.23 m²) |
| Radar, E-M Band (2-100 GHz) | -2.1 dBsm (0.6166 m²) | 0.2 dBsm (1.05 m²) | -2.1 dBsm (0.6166 m²) |
Default Configuration
| Model | Comments |
|---|
Datalink
| Type | Model | Range | Channels |
|---|---|---|---|
| Radio | SHF 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 Rotax 914 UL | Piston | 1 | 85 | - | 1.25 | - | No | - |
Fuel
| Fuel Type | Fuel Capacity |
|---|---|
| Aviation Fuel | 387 |