1. Taiwan
  2. Aircraft
  3. Chung Shyang II [Albatross] UAV

Basic Information

Category Fixed Wing Type Unmanned Aerial Vehicle (UAV)
Year Commissioned 2011 Year Decommissioned 0
Agility 1 Damage Points (DP) 3
Empty Weight 320 kg Max Weight 465 kg
Runway Information 250-450m (STOL) TOD/LAD Physical Size UAS [NATO Class II] (150-600kg)
Cost 0 Hypothetical No
Payload Weight 55 kg Crew 0 people

Aircraft Capabilities

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

Sensor Parameters

Model Purpose Range Scan Interval Generation
Albatross EO Payload [IR/TV/Laser Rangefinder] Sensor Group
Group Components
# Component Type Purpose Range Scan Interval Generation
1 Albatross EO Payload [IR] Infrared Infrared, Target Search, Tracking and Identification Camera 0.00 - 8.00 nm 10 sec Infrared, 3rd Generation Imaging (2000s/2010s, Impr LANTIRN, Litening II/III, ATFLIR)
2 Albatross EO Payload [TV Camera] Visual Visual, Target Search, Tracking and Identification TV Camera 0.00 - 8.00 nm 10 sec Visual, 3rd Generation TV Camera (2000s/2010s, CCD)
3 Albatross EO Payload [Laser Rangefinder] Laser Rangefinder Laser Rangefinder 0.00 - 8.00 nm 0 sec Not Applicable (N/A)

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
Albatross EO Payload [IR/TV/Laser Rangefinder] 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
No Data

Signatures

Type Front Side Rear
Visual Detection Range 1.5 nm 2.3 nm 1.5 nm
Visual Classification Range 0.93 nm 1.53 nm 1.38 nm
Infrared Detection Range 1.5 nm 4.12 nm 10.05 nm
Infrared Classification Range 0.93 nm 1.53 nm 0.93 nm
Radar, A-D Band (30-2000 MHz) -4.6 dBsm (0.3467 m²) -2 dBsm (0.6310 m²) -4.6 dBsm (0.3467 m²)
Radar, E-M Band (2-100 GHz) -7.6 dBsm (0.1738 m²) -5 dBsm (0.3162 m²) -7.6 dBsm (0.1738 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 NCSIST RU 260 Piston 1 38 - 1.25 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 90