Basic Information

Category Fixed Wing Type Target Drone
Year Commissioned 1981 Year Decommissioned 0
Agility 1 Damage Points (DP) 3
Empty Weight 4200 kg Max Weight 4200 kg
Runway Information 0m (VTOL) TOD/LAD Physical Size Small Aircraft (0-12m)
Cost 0 Hypothetical No
Payload Weight 0 kg Crew 0 people

Aircraft Capabilities

Blip Enhance / Luneberg Reflectors Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles) Fuselage Structure - High Supersonic Fighter

Sensor Parameters

Model Purpose Range Scan Interval Generation
SPS-61R/63R Azaliya OECM, Offensive ECM 0.00 - 0.00 nm 0 sec Late 1970s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
SPS-61R/63R Azaliya SB1, SB2, SMF1, SMF2, SMA1, SMA2, SS1, SS2, PB1, PB2, PMF1, PMF2, PMA1, PMA2, PS1, PS2

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 2.32 nm 4.73 nm 2.32 nm
Visual Classification Range 1.14 nm 2.39 nm 1.7 nm
Infrared Detection Range 1.55 nm 5.08 nm 10.16 nm
Infrared Classification Range 0.95 nm 1.99 nm 0.95 nm
Radar, A-D Band (30-2000 MHz) -1.3 dBsm (0.7413 m²) 1.3 dBsm (1.35 m²) -1.3 dBsm (0.7413 m²)
Radar, E-M Band (2-100 GHz) -1.3 dBsm (0.7413 m²) 1.3 dBsm (1.35 m²) -1.3 dBsm (0.7413 m²)

Default Configuration

Model Comments
No Data

Datalink

Type Model Range Channels
Radio HF Radio [Secure] 300 nm 10

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
RD-9FK Rocket Sustainer Turbojet - 1 - 1 - No Aircraft Implementation

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 664