1. Switzerland
  2. Aircraft
  3. AS.332M1 Super Puma [TH06]

Basic Information

Category Helicopter Type Search And Rescue (SAR)
Year Commissioned 1987 Year Decommissioned 0
Agility 1 Damage Points (DP) 5
Empty Weight 4330 kg Max Weight 8600 kg
Runway Information 0m (VTOL) TOD/LAD Physical Size Medium Aircraft (12.1-18m)
Cost 0 Hypothetical No
Payload Weight 0 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
Generic IR Camera Infrared, Surveillance Camera 0.00 - 30.00 nm 10 sec Infrared, 3rd Generation Imaging (2000s/2010s, Impr LANTIRN, Litening II/III, ATFLIR)

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
Generic IR Camera SB1, SB2, SMF1, SMF2, SMA1, SMA2, PB1, PB2, PMF1, PMF2, PMA1, PMA2 否

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 1.98 nm 5.8 nm 1.98 nm
Visual Classification Range 0.99 nm 2.81 nm 1.55 nm
Infrared Detection Range 1.98 nm 7.63 nm 11.19 nm
Infrared Classification Range 1.17 nm 3.31 nm 1.17 nm
Radar, A-D Band (30-2000 MHz) 1.7 dBsm (1.48 m²) 4.2 dBsm (2.63 m²) 1.7 dBsm (1.48 m²)
Radar, E-M Band (2-100 GHz) 1.7 dBsm (1.48 m²) 4.2 dBsm (2.63 m²) 1.7 dBsm (1.48 m²)

Default Configuration

Model Comments
No Data

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
2x Makila 1A1 Helo Turboshaft 2 1877 - 0.481 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 1360