1. Israel
  2. Aircraft
  3. Mastiff UAV

Basic Information

Category Fixed Wing Type Unmanned Aerial Vehicle (UAV)
Year Commissioned 1978 Year Decommissioned 1992
Agility 0.5 Damage Points (DP) 3
Empty Weight 72 kg Max Weight 138 kg
Runway Information 250-450m (STOL) TOD/LAD Physical Size UAS [NATO Class I, Small] (20-150kg)
Cost 0 Hypothetical No
Payload Weight 37 kg Crew 0 people

Aircraft Capabilities

No Data

Sensor Parameters

Model Purpose Range Scan Interval Generation
Generic TV Camera Visual, Surveillance TV Camera 0.00 - 30.00 nm 10 sec Visual, 2nd Generation TV Camera (1980s/1990s, AXX-1 TCS)

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
Generic TV Camera 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 0.87 nm 1.4 nm 0.87 nm
Visual Classification Range 0.59 nm 1.01 nm 0.8 nm
Infrared Detection Range 0.87 nm 2.96 nm 8.13 nm
Infrared Classification Range 0.59 nm 1.01 nm 0.59 nm
Radar, A-D Band (30-2000 MHz) -8.1 dBsm (0.1549 m²) -5.3 dBsm (0.2951 m²) -8.1 dBsm (0.1549 m²)
Radar, E-M Band (2-100 GHz) -8.1 dBsm (0.1549 m²) -5.3 dBsm (0.2951 m²) -8.1 dBsm (0.1549 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 Piston Engine Piston 1 22 - 1.25 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 35