1. Kuwait
  2. Aircraft
  3. SA.330F Puma

Basic Information

Category Helicopter Type Utility
Year Commissioned 1976 Year Decommissioned 0
Agility 1 Damage Points (DP) 5
Empty Weight 3715 kg Max Weight 7500 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
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
Trooper   x 20

Signatures

Type Front Side Rear
Visual Detection Range 1.85 nm 5.5 nm 1.85 nm
Visual Classification Range 1.1 nm 3.16 nm 1.7 nm
Infrared Detection Range 1.85 nm 7.36 nm 10.89 nm
Infrared Classification Range 1.1 nm 3.16 nm 1.1 nm
Radar, A-D Band (30-2000 MHz) 0.9 dBsm (1.23 m²) 3.4 dBsm (2.19 m²) 0.9 dBsm (1.23 m²)
Radar, E-M Band (2-100 GHz) 0.9 dBsm (1.23 m²) 3.4 dBsm (2.19 m²) 0.9 dBsm (1.23 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 Turmo IVA Helo Turboshaft 2 1417 - 0.629 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 1240