1. United States
  2. Aircraft
  3. X-61A Gremlin

Basic Information

Category Fixed Wing Type Unmanned Aerial Vehicle (UAV)
Year Commissioned 0 Year Decommissioned 0
Agility 1 Damage Points (DP) 3
Empty Weight 615 kg Max Weight 680 kg
Runway Information Catapult Launcher Physical Size UAS [NATO Class II] (150-600kg)
Cost 0 Hypothetical Yes
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
No Data

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
No Data

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 0.88 nm 1.55 nm 0.88 nm
Visual Classification Range 0.59 nm 1.1 nm 0.81 nm
Infrared Detection Range 0.88 nm 3.17 nm 8.16 nm
Infrared Classification Range 0.59 nm 1.1 nm 0.59 nm
Radar, A-D Band (30-2000 MHz) -11.1 dBsm (0.0776 m²) -8.2 dBsm (0.1514 m²) -11.1 dBsm (0.0776 m²)
Radar, E-M Band (2-100 GHz) -14.1 dBsm (0.0389 m²) -11.2 dBsm (0.0759 m²) -14.1 dBsm (0.0389 m²)

Default Configuration

Model Comments
No Data

Datalink

Type Model Range Channels
No Data

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
1x F107-WR-402 Turbofan 1 5245 - 0.63 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 35