Basic Information

Category Fixed Wing Type Unmanned Aerial Vehicle (UAV)
Year Commissioned 1972 Year Decommissioned 1990
Agility 0.5 Damage Points (DP) 3
Empty Weight 78 kg Max Weight 156 kg
Runway Information Catapult Launcher Physical Size UAS [NATO Class II] (150-600kg)
Cost 0 Hypothetical No
Payload Weight 30 kg Crew 0 people

Aircraft Capabilities

Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles)

Sensor Parameters

Model Purpose Range Scan Interval Generation
Generic TV Camera Visual, Surveillance TV Camera 0.00 - 15.00 nm 10 sec Visual, 1st Generation TV Camera (1960s/1970s, TISEO)
Generic Infrared Line Scanner (IRLS) IRLS, Non-Imaging Infrared Line Scanner 0.00 - 5.00 nm 10 sec Infrared, Non-Imaging

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
Generic TV Camera SB1, SB2, SMF1, SMF2, SMA1, SMA2, PB1, PB2, PMF1, PMF2, PMA1, PMA2
Generic Infrared Line Scanner (IRLS) SB1, SB2, SMF1, SMF2, SMA1, SMA2, PB1, PB2, PMF1, PMF2, PMA1, PMA2

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
No Data
No Data
No Data
No Data

Signatures

Type Front Side Rear
Visual Detection Range 0.56 nm 1.64 nm 0.56 nm
Visual Classification Range 0.41 nm 1.15 nm 0.51 nm
Infrared Detection Range 0.56 nm 3.29 nm 6.85 nm
Infrared Classification Range 0.41 nm 1.15 nm 0.41 nm
Radar, A-D Band (30-2000 MHz) -13.5 dBsm (0.0447 m²) -10.4 dBsm (0.0912 m²) -13.5 dBsm (0.0447 m²)
Radar, E-M Band (2-100 GHz) -13.5 dBsm (0.0447 m²) -10.4 dBsm (0.0912 m²) -13.5 dBsm (0.0447 m²)

Default Configuration

Model Comments
No Data

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 WI WR2-6 Turbojet Turbojet 1 125 - 1.25 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 65