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The Sikorsky SH-60/MH-60 Seahawk (or Sea Hawk) is a twin turboshaft engine, multi-mission United States Navy helicopter based on the United States Army UH-60 Black Hawk and a member of the Sikorsky S-70 family. The most significant airframe modification is a hinged tail to reduce its footprint aboard ships.
The U.S. Navy uses the H-60 airframe under the model designations SH-60B, SH-60F, HH-60H, MH-60R, and MH-60S. Able to deploy aboard any air-capable frigate, destroyer, cruiser, fast combat support ship,amphibious assault ship, or aircraft carrier, the Seahawk can handle anti-submarine warfare (ASW), anti-surface warfare (ASUW), naval special warfare (NSW) insertion, search and rescue (SAR), combat search and rescue (CSAR), vertical replenishment (VERTREP), and medical evacuation (MEDEVAC). All Navy H-60s carry a rescue hoist for SAR/CSAR missions.
General characteristics
Performance
Armament
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Server: Esterlon Community Server
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Built by: Kroindaal
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Refrence: https://en.wikipedia.org/wiki/SH-60_Seahawk
Time: ~45 minutes
This work by Kroindaal is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.
Based on a work at http://esterlon.enjin.com/home.
Permissions beyond the scope of this license may be available at Kroindaal's PMC.
The U.S. Navy uses the H-60 airframe under the model designations SH-60B, SH-60F, HH-60H, MH-60R, and MH-60S. Able to deploy aboard any air-capable frigate, destroyer, cruiser, fast combat support ship,amphibious assault ship, or aircraft carrier, the Seahawk can handle anti-submarine warfare (ASW), anti-surface warfare (ASUW), naval special warfare (NSW) insertion, search and rescue (SAR), combat search and rescue (CSAR), vertical replenishment (VERTREP), and medical evacuation (MEDEVAC). All Navy H-60s carry a rescue hoist for SAR/CSAR missions.
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 or 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
Role | Multimission maritime helicopter |
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Manufacturer | Sikorsky Aircraft |
First flight | 12 December 1979 |
Introduction | 1984 |
Status | In service |
Primary users | United States Navy Royal Australian Navy |
Produced | 1979–present |
Unit cost | US$42.9m (MH-60R in FY2012)[1] US$28.1m (MH-60S in FY2012)[2] |
Developed from | Sikorsky UH-60 Black Hawk |
Variants | Sikorsky HH-60 Jayhawk Mitsubishi SH-60 |
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Server: Esterlon Community Server
P: 37.187.128.234:27260I
Built by: Kroindaal
---
Refrence: https://en.wikipedia.org/wiki/SH-60_Seahawk
Time: ~45 minutes
This work by Kroindaal is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.
Based on a work at http://esterlon.enjin.com/home.
Permissions beyond the scope of this license may be available at Kroindaal's PMC.
Progress | 100% complete |
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