1. United States
  2. Aircraft
  3. MH-60S Seahawk

Basic Information

Category Helicopter Type Transport
Year Commissioned 2016 Year Decommissioned 0
Agility 1 Damage Points (DP) 5
Empty Weight 6190 kg Max Weight 9927 kg
Runway Information 0m (VTOL) TOD/LAD Physical Size Medium Aircraft (12.1-18m)
Cost 0 Hypothetical No
Payload Weight 4080 kg Crew 4 people

Aircraft Capabilities

HIFR Capable Nap-of-the-Earth (NOE) Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles) IRSS - Shielded Exhaust (Jet Deviation)

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
Trooper   x 12
750 liter Ferry Tank   x 2

Signatures

Type Front Side Rear
Visual Detection Range 1.66 nm 5.22 nm 1.66 nm
Visual Classification Range 0.93 nm 2.81 nm 1.43 nm
Infrared Detection Range 1.84 nm 7.63 nm 10.87 nm
Infrared Classification Range 1.1 nm 3.31 nm 1.1 nm
Radar, A-D Band (30-2000 MHz) 0.8 dBsm (1.20 m²) 3.3 dBsm (2.14 m²) 0.8 dBsm (1.20 m²)
Radar, E-M Band (2-100 GHz) 0.8 dBsm (1.20 m²) 3.3 dBsm (2.14 m²) 0.8 dBsm (1.20 m²)

Default Configuration

Model Comments

Datalink

Type Model Range Channels
Radio AN/ARC-174 HF Communications [Commercial 718U] 300 nm 0

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
2x T700-GE-401C Helo Turboshaft 2 1720 - 0.464 - No MCM, 30kt loiter

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 1810