1. India
  2. Aircraft
  3. SA.316B Chetak MATCH [ASW, Alouette III]

Basic Information

Category Helicopter Type Anti-Submarine Warfare (ASW)
Year Commissioned 1974 Year Decommissioned 0
Agility 1 Damage Points (DP) 3
Empty Weight 1143 kg Max Weight 2200 kg
Runway Information 0m (VTOL) TOD/LAD Physical Size Small Aircraft (0-12m)
Cost 0 Hypothetical No
Payload Weight 750 kg Crew 2 people

Aircraft Capabilities

Nap-of-the-Earth (NOE) Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles)

Sensor Parameters

Model Purpose Range Scan Interval Generation
ORB 31S2 Heracles I Radar, Surface Search, Medium-Range 0.40 - 60.00 nm 5 sec Late 1970s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
ORB 31S2 Heracles I 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
Mk44 Mod 1   x 2
Mk44 Mod 1   x 1
Generic MAD Pod   x 1

Signatures

Type Front Side Rear
Visual Detection Range 1.42 nm 3.87 nm 1.42 nm
Visual Classification Range 0.88 nm 2.36 nm 1.3 nm
Infrared Detection Range 1.42 nm 5.82 nm 9.82 nm
Infrared Classification Range 0.88 nm 2.36 nm 0.88 nm
Radar, A-D Band (30-2000 MHz) -2.3 dBsm (0.5888 m²) 0.3 dBsm (1.07 m²) -2.3 dBsm (0.5888 m²)
Radar, E-M Band (2-100 GHz) -2.3 dBsm (0.5888 m²) 0.3 dBsm (1.07 m²) -2.3 dBsm (0.5888 m²)

Default Configuration

Model Comments

Datalink

Type Model Range Channels
Radio UHF/VHF Radio [Secure] 100 nm 0

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
1x Astazou XIVA Helo Turboshaft 1 600 - 0.53 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 460