Basic Information

Category Fixed Wing Type Attack
Year Commissioned 1962 Year Decommissioned 1995
Agility 3 Damage Points (DP) 3
Empty Weight 3100 kg Max Weight 5500 kg
Runway Information 451-900m TOD/LAD Physical Size Small Aircraft (0-12m)
Cost 0 Hypothetical No
Payload Weight 500 kg Crew 1 people

Aircraft Capabilities

Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles) Bombsight - Basic Probe Refueling

Sensor Parameters

Model Purpose Range Scan Interval Generation
Generic Visual Reconnaissance Camera Visual, Reconnaissance Frame Camera 0.00 - 5.00 nm 10 sec Visual
Generic Visual Reconnaissance Camera Visual, Reconnaissance Frame Camera 0.00 - 5.00 nm 10 sec Visual
Generic Visual Reconnaissance Camera Visual, Reconnaissance Frame Camera 0.00 - 5.00 nm 10 sec Visual

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
Generic Visual Reconnaissance Camera SB1, SB2, PB1, PB2
Generic Visual Reconnaissance Camera PMF1, PMF2, PMA1, PMA2
Generic Visual Reconnaissance Camera SMF1, SMF2, SMA1, SMA2

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius

Signatures

Type Front Side Rear
Visual Detection Range 1.98 nm 4.22 nm 1.98 nm
Visual Classification Range 1.17 nm 2.54 nm 1.82 nm
Infrared Detection Range 1.98 nm 6.17 nm 11.19 nm
Infrared Classification Range 1.17 nm 2.54 nm 1.17 nm
Radar, A-D Band (30-2000 MHz) 1.7 dBsm (1.48 m²) 4.2 dBsm (2.63 m²) 1.7 dBsm (1.48 m²)
Radar, E-M Band (2-100 GHz) 1.7 dBsm (1.48 m²) 4.2 dBsm (2.63 m²) 1.7 dBsm (1.48 m²)

Default Configuration

Model Comments
12.7mm/50 MG x 4 [300 rnds x 4] Aircraft, G.91R/1

Datalink

Type Model Range Channels
Radio VHF Radio [Unsecure] 100 nm 0
Radio UHF 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 Orpheus BOr.803 Turbojet 1 2270 - 1.08 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 1290