1. India
  2. Aircraft
  3. Ajeet Mk1

Basic Information

Category Fixed Wing Type Attack
Year Commissioned 1978 Year Decommissioned 1991
Agility 3 Damage Points (DP) 3
Empty Weight 2307 kg Max Weight 4173 kg
Runway Information 451-900m TOD/LAD Physical Size Small Aircraft (0-12m)
Cost 0 Hypothetical No
Payload Weight 900 kg Crew 1 people

Aircraft Capabilities

Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles) Bombsight - Ballistic Computing

Sensor Parameters

Model Purpose Range Scan Interval Generation

Sensor Coverage Diagram
Model Detection Angle Omnidirectional

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
250kg GPB   x 4
250kg GPB   x 2

Signatures

Type Front Side Rear
Visual Detection Range 1.68 nm 3.46 nm 1.68 nm
Visual Classification Range 1.02 nm 2.15 nm 1.54 nm
Infrared Detection Range 1.68 nm 5.41 nm 10.49 nm
Infrared Classification Range 1.02 nm 2.15 nm 1.02 nm
Radar, A-D Band (30-2000 MHz) -0.3 dBsm (0.9333 m²) 2.3 dBsm (1.70 m²) -0.3 dBsm (0.9333 m²)
Radar, E-M Band (2-100 GHz) -0.3 dBsm (0.9333 m²) 2.3 dBsm (1.70 m²) -0.3 dBsm (0.9333 m²)

Default Configuration

Model Comments
30mm ADEN Mk4 x 2 [90 rnds x 2] Aircraft, Ajeet

Datalink

Type Model Range Channels
Radio VHF Radio [Unsecure] 100 nm 0
Radio UHF 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 Orpheus BOr.2 Mk701-01 Turbojet 1 2133 - 1.1 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 1275