1. United States
  2. Aircraft
  3. RQ-1A Predator UAV

Basic Information

Category Fixed Wing Type Unmanned Aerial Vehicle (UAV)
Year Commissioned 1995 Year Decommissioned 1996
Agility 1 Damage Points (DP) 3
Empty Weight 513 kg Max Weight 1020 kg
Runway Information 250-450m (STOL) TOD/LAD Physical Size Small Aircraft (0-12m)
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
Wescam 14TS [IR] Infrared, Surveillance Camera 0.00 - 30.00 nm 10 sec Infrared, 2nd Generation Imaging (1980s/1990s, LANTIRN, Litening) )

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
Wescam 14TS [IR] 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 2.13 nm 2.82 nm 2.13 nm
Visual Classification Range 1.15 nm 1.69 nm 1.84 nm
Infrared Detection Range 2.37 nm 5.07 nm 11.99 nm
Infrared Classification Range 1.36 nm 1.98 nm 1.36 nm
Radar, A-D Band (30-2000 MHz) 0.9 dBsm (1.23 m²) 3.2 dBsm (2.09 m²) 0.9 dBsm (1.23 m²)
Radar, E-M Band (2-100 GHz) -2.1 dBsm (0.6166 m²) 0.2 dBsm (1.05 m²) -2.1 dBsm (0.6166 m²)

Default Configuration

Model Comments
No Data

Datalink

Type Model Range Channels
Radio UHF/VHF Radio [Unsecure] 100 nm 0
MILSTAR SATCOM MILSTAR SATCOM 0 nm 0

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
1x Rotax 912 UL Piston 1 85 - 1.25 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 387