Sikorsky SH-60 Seahawk - Specifications (SH-60B)

Specifications (SH-60B)

Data from Brassey's World Aircraft & Systems Directory, Navy fact file, and Sikorsky S-70B

General characteristics

  • Crew: 3–4
  • Capacity: 5 passengers in cabin, slung load of 6,000 lb (2,700 kg) or internal load of 4,100 lb (1,900 kg) for B, F and H models; and 11 passengers or slung load of 9,000 lb (4,100 kg) for S-model
  • Length: 64 ft 8 in (19.75 m)
  • Rotor diameter: 53 ft 8 in (16.35 m)
  • Height: 17 ft 2 in (5.2 m)
  • Disc area: 2,262 ft² (210 m²)
  • Empty weight: 15,200 lb (6,895 kg)
  • Loaded weight: 17,758 lb (8,055 kg) ; for ASW mission
  • Useful load: 6,684 lb (3,031 kg)
  • Max. takeoff weight: 21,884 lb (9,927 kg)
  • Powerplant: 2 × General Electric T700-GE-401C turboshaft, 1,890 shp (1,410 kW) take-off power each

Performance

  • Never exceed speed: 180 kn (333 km/h; 207 mph)
  • Maximum speed: 146 kn (270 km/h; 168 mph)
  • Range: 450 nmi (518 mi/834 km) at cruise speed
  • Service ceiling: 12,000 ft (3,580 m)
  • Rate of climb: 1,650 ft/min (8.38 m/s)

Armament

  • Up to three Mark 46 torpedos or Mk-54s,
  • AGM-114 Hellfire missile, 4 Hellfire missiles for SH-60B and HH-60H and MH-60R, 8 Hellfire missiles for MH-60S Block III.
  • AGM-119 Penguin missile (being phased out),
  • M60 machine gun or, M240 machine gun or GAU-16/A machine gun or GAU-17/A Minigun
  • Rapid Airborne Mine Clearance System (RAMICS) using Mk 44 Mod 0 30 mm Cannon
Main article: U.S. Helicopter Armament Subsystems

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