1. United States
  2. Aircraft
  3. F-106A Delta Dart

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
No Data
No Data

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