1. United States
  2. Aircraft
  3. UC-35A [Cessna 560 Citation Ultra]

Basic Information

Category Fixed Wing Type Transport
Year Commissioned 1999 Year Decommissioned 0
Agility 1 Damage Points (DP) 3
Empty Weight 4261 kg Max Weight 7394 kg
Runway Information 901-1400m TOD/LAD Physical Size Medium Aircraft (12.1-18m)
Cost 0 Hypothetical No
Payload Weight 0 kg Crew 2 people

Aircraft Capabilities

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

Sensor Parameters

Model Purpose Range Scan Interval Generation
AN/AAR-57 CMWS MAWS, Missile Approach Warning System 0.00 - 5.00 nm 60 sec Late 2000s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
AN/AAR-57 CMWS SB1, SB2, SMF1, SMF2, SMA1, SMA2, SS1, SS2, PB1, PB2, PMF1, PMF2, PMA1, PMA2, PS1, PS2 是

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
No Data
No Data
No Data
Passenger   x 10

Signatures

Type Front Side Rear
Visual Detection Range 4.62 nm 8.35 nm 4.62 nm
Visual Classification Range 2.02 nm 3.84 nm 3.39 nm
Infrared Detection Range 3.08 nm 7.42 nm 13.28 nm
Infrared Classification Range 1.69 nm 3.2 nm 1.69 nm
Radar, A-D Band (30-2000 MHz) 7 dBsm (5.01 m²) 9.3 dBsm (8.51 m²) 7 dBsm (5.01 m²)
Radar, E-M Band (2-100 GHz) 7 dBsm (5.01 m²) 9.3 dBsm (8.51 m²) 7 dBsm (5.01 m²)

Default Configuration

Model Comments
AN/ALE-47 CMDS x 2 [60 Cartridges] USN, Dual Spectral, Chaff & Flare Dispenser

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
2x JT15D-5A Turbofan 2 1382 - 0.562 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 2640