Basic Information

Category Fixed Wing Type Unmanned Aerial Vehicle (UAV)
Year Commissioned 1964 Year Decommissioned 1983
Agility 1 Damage Points (DP) 20
Empty Weight 11450 kg Max Weight 35610 kg
Runway Information Catapult Launcher Physical Size Very Large Aircraft (26.1-75m)
Cost 0 Hypothetical No
Payload Weight 0 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 Visual Reconnaissance Camera Visual, Reconnaissance Frame Camera 0.00 - 5.00 nm 10 sec Visual
SRS-6RD Romb-4A COMINT 0.00 - 500.00 nm 20 sec Late 1970s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
Generic Visual Reconnaissance Camera SB1, SB2, SMF1, SMF2, SMA1, SMA2, SS1, SS2, PB1, PB2, PMF1, PMF2, PMA1, PMA2, PS1, PS2
SRS-6RD Romb-4A 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 3.56 nm 8.85 nm 3.56 nm
Visual Classification Range 1.9 nm 4.7 nm 3.26 nm
Infrared Detection Range 3.56 nm 10.11 nm 14.05 nm
Infrared Classification Range 1.9 nm 4.7 nm 1.9 nm
Radar, A-D Band (30-2000 MHz) 8.8 dBsm (7.59 m²) 11 dBsm (12.59 m²) 8.8 dBsm (7.59 m²)
Radar, E-M Band (2-100 GHz) 8.8 dBsm (7.59 m²) 11 dBsm (12.59 m²) 8.8 dBsm (7.59 m²)

Default Configuration

Model Comments
No Data

Datalink

Type Model Range Channels
Radio UHF/VHF Radio [Unsecure] 100 nm 0
Radio HF Radio [Unsecure] 300 nm 10

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
1x KR-15-300 Turbojet 1 10000 - 2 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 16600