Basic Information
| Category | Fixed Wing | Type | Fighter |
| Year Commissioned | 1968 | Year Decommissioned | 1988 |
| Agility | 3 | Damage Points (DP) | 10 |
| Empty Weight | 10735 kg | Max Weight | 17350 kg |
| Runway Information | 901-1400m TOD/LAD | Physical Size | Large Aircraft (18.1-26m) |
| Cost | 0 | Hypothetical | No |
| Payload Weight | 0 kg | Crew | 1 people |
Aircraft Capabilities
Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles)
Boom Refueling
Sensor Parameters
| Model | Purpose | Range | Scan Interval | Generation |
| MA-1 | Radar, FCR, Air-to-Air, Short-Range | 0.20 - 40.00 nm | 2 sec | Early 1960s |
| Generic IRST | IRST, Non-Imaging Infrared Search and Track | 0.00 - 30.00 nm | 10 sec | Infrared, Non-Imaging |
Sensor Coverage Diagram
| Model | Detection Angle | Omnidirectional |
| MA-1 | SB1, PB2 | 否 |
| Generic IRST | SB1, PB2 | 否 |
Weapon Loadouts Click to Expand Beta
| Loadout Type | Role | Ready Time | Combat Radius | |||
|---|---|---|---|---|---|---|
| (Ferry) | Ferry | 30 min | 1900 nm | |||
| (Reserve [Available]) | Reserve | 180 min | 0 nm | |||
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| (Maintenance [Unavailable]) | Unavailable | 0 min | 0 nm | |||
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| A/A: AIM-4G Falcon | Air Superiority, WVR AAMs | 180 min | 200 nm | |||
| A/A: AIM-4G Falcon, Long-Range | Air Superiority, WVR AAMs | 180 min | 200 nm | |||
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| A/A: AIM-4G Falcon, AIR-2A Genie [1.5kT Nuclear] | Air Superiority, WVR AAMs | 180 min | 200 nm | |||
| A/A: AIM-4G Falcon, AIR-2A Genie [1.5kT Nuclear], Long-Range | Air Superiority, WVR AAMs | 180 min | 200 nm | |||
Signatures
| Type | Front | Side | Rear |
|---|---|---|---|
| Visual Detection Range | 3.3 nm | 7.82 nm | 3.3 nm |
| Visual Classification Range | 1.79 nm | 4.24 nm | 3.03 nm |
| Infrared Detection Range | 3.3 nm | 9.31 nm | 13.64 nm |
| Infrared Classification Range | 1.79 nm | 4.24 nm | 1.79 nm |
| Radar, A-D Band (30-2000 MHz) | 7.9 dBsm (6.17 m²) | 10.1 dBsm (10.23 m²) | 7.9 dBsm (6.17 m²) |
| Radar, E-M Band (2-100 GHz) | 7.9 dBsm (6.17 m²) | 10.1 dBsm (10.23 m²) | 7.9 dBsm (6.17 m²) |
Default Configuration
| Model | Comments |
|---|---|
| 20mm/85 M61A1 Vulcan [650 rnds] | Aircraft, F-106A |
Datalink
| Type | Model | Range | Channels |
|---|---|---|---|
| Radio | UHF/VHF Radio [Unsecure] | 100 nm | 0 |
Engines
| Model | Type | Engine Count | Military Thrust | Afterburner Thrust | Military Fuel Rate (SFC) | Afterburner Fuel Rate (SFC) | Hypothetical | Comments |
|---|---|---|---|---|---|---|---|---|
| 1x J75-PW-17 | Turbojet | 1 | 7800 | 11123 | 0.85 | 2.15 | No | - |
Fuel
| Fuel Type | Fuel Capacity |
|---|---|
| Aviation Fuel | 4410 |