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Encyclopedia - Sikorsky H-60 Blackhawk/Seahawk

During the 1970s the U.S. Navy began looking for new helicopter to replace the Kaman SH-2 Seasprite. The SH-2 Seasprite was used by the Navy as its platform for the Light Airborne Multi-Purpose System (LAMPS) Mark I avionics suite for the maritime warfare and a secondary search and rescue capability. Advances in sensor and avionic technology lead to LAMPS Mk II suite, but the SH-2 was not large enough to carry the Navy required equipment. In the mid-1970s the Army was evaluating of the Sikorsky YUH-60 and Boeing-Vertol YUH-61 for its Utility Tactical Transport Aircraft System (UTTAS) competition.

The Navy based its requirements on the Army UTTAS specification to decrease costs from commonality.[2] Sikorsky and Boeing-Vertol submitted proposals for Navy versions of their Army UTTAS helicopters in April 1977 for review. The Navy also looked at helicopters being produced by Bell, Kaman, Westland and MBB, but these were too small for the mission. In early 1978 the Navy selected Sikorsky S-70B design, which was designated SH-60B Seahawk.

SH-60B Seahawk

The SH-60B maintained 83% commonality with the UH-60A. The main changes made included corrosion protection, more powerful T700 engines, single-stage oleo main landing gear, replacing left side door with fuselage structure, adding two weapon pylons, and shifting the tail landing gear 13 feet (3.96 m) forward to reduce the footprint for shipboard landing. Other changes included larger fuel cells, an electric blade folding system, folding horizontal stabilators for storage, and adding a 25-tube pneumatic sonobuoy launcher on left side. An emergency flotation system was also installed in the stub wing fairings of the main landing gear on both sides of the aircraft.

Five YSH-60B Seahawk LAMPS III prototypes were ordered. The first flight of a YSH-60B occurred on 12 December 1979. The first production version SH-60B achieved its first flight on 11 February 1983. The SH-60B entered operational service in 1984 with first operational deployment in 1985.

The SH-60B LAMPS Mk III is deployed primarily aboard frigates, destroyers, and cruisers. The primary missions of the SH-60B are surface warfare and anti-submarine warfare.

The SH-60B carries a complex system of sensors including a towed Magnetic Anomaly Detector (MAD) and air-launched sonobuoys. Other sensors include the APS-124 search radar, ALQ-142 ESM system and optional nose-mounted forward looking infrared (FLIR) turret. It carries the Mk 46, Mk 50, or Mk 54 torpedo, AGM-114 Hellfire missile, and a single cabin-door-mounted M60D/M240 7.62 mm (0.30 in) machine gun or GAU-16 .50 in (12.7 mm) machine gun.

A standard crew for a SH-60B is one pilot, one ATO/Co-Pilot (Airborne Tactical Officer), and an enlisted aviation warfare systems operator (sensor operator). Operating squadrons are designated Helicopter Anti-Submarine Squadron, Light (HSL).

The SH-60J is a version of the SH-60B for the Japan Maritime Self-Defense Force. The SH-60K is a modified version of the SH-60J. The SH-60J and SH-60K are built under license by Mitsubishi in Japan.

SH-60F Seahawk

After the SH-60B entered service, the Navy began development of the SH-60F variant to replace the SH-3 Sea King. Development of this variant began with the award of a contract to Sikorsky in March 1985. An early SH-60B was modified to serve as a SH-60F prototype. The company was contracted to produce seven SH-60Fs in January 1986 and the first example flew on 19 March 1987.

The SH-60F serves as the carrier battle group\'s primary anti-submarine warfare (ASW) and search and rescue (SAR) aircraft. It hunts submarines with the AN/AQS-13F dipping sonar, and carries 14 sonobuoys. The SH-60F is unofficially called the \"Oceanhawk\". The SH-60F can carry the Mk 46, MK 50, or MK 54 torpedo and a choice of cabin-mounted machine guns, including the M60D, M240D, and GAU-16 (50 CAL) for defense. Standard crew complement is one pilot, one copilot, one enlisted tactical sensor operator (TSO), and one enlisted acoustic sensor operator (ASO).

HH-60H Seahawk

The HH-60H was developed beginning in September 1986 with a contract for the first five helicopters. The variant\'s first flight occurred on 17 August 1988. The HH-60H was developed in conjunction with the US Coast Guard\'s HH-60J. Deliveries of the HH-60H began in 1989. The variant earned initial operating capability in April 1990. The HH-60H\'s official DoD and Sikorsky name is Seahawk, though it has been called \"Rescue Hawk\".

Based on the SH-60F, the HH-60H is the primary combat search and rescue (CSAR), naval special warfare (NSW) and anti-surface warfare (ASUW) helicopter. It carries a variety of defensive and offensive sensors making it one of the most survivable helicopters in the world. Sensors include a FLIR turret with laser designator and the Aircraft Survival Equipment (ASE) package including the ALQ-144 Infrared Jammer, AVR-2 Laser Detectors, APR-39(V)2 Radar Detectors, AAR-47 Missile Launch Detectors and ALE-47 chaff/flare dispensers. Additionally, airframe improvements in engine exhaust deflectors provide infrared thermal reduction reducing the threat of heat-seeking missiles. The HH-60H can carry up to four AGM-114 Hellfire missiles on an extended wing using the M299 launcher and a variety of cabin and port window mounted guns including M60D, M240, GAU-16 and GAU-17/A machine guns.

The HH-60H\'s standard crew is pilot, copilot, an enlisted crew chief, and two door gunners. The HH-60H is operated by Helicopter Antisubmarine (HS) squadrons with a standard dispersal of four F-models and three H-models. In Iraq, HH-60Hs were used by the Navy, assisting the Army, for MEDEVAC purposes and special operations missions.[citation needed] As the Navy transitions its Helicopter Antisubmarine (HS) squadrons to the MH-60S, remaining HH-60Hs are being transferred to its East and West coast special operations squadrons (HSC-84 and HSC-85, respectively).

MH-60S \"Knighthawk\"

The Navy decided to replace its venerable CH-46 Sea Knight helicopters in 1997. After sea demonstrations by a converted UH-60, the Navy awarded production contract for the CH-60S in 1998. The variant first flew in 27 January 2000 and it began flight testing later that year. The CH-60S was redesignated MH-60S in February 2001 to reflect its planned multi-mission use.

The MH-60S is based on the UH-60L and has many naval SH-60 features. Unlike all other Navy H-60s, the MH-60S is not based on the original S-70B/SH-60B platform with its forward-mounted twin tail-gear and single starboard sliding cabin door. Instead, the S-model is a hybrid, featuring the main fuselage of the S-70A/UH-60, with large sliding doors on both sides of the cabin and a single aft-mounted tail wheel; and the engines, drivetrain and rotors of the S-70B/SH-60.

It is deployed aboard amphibious assault ships and fast combat supply ships. It has two missions: troop transport and vertical replenishment (VERTREP), but can also perform search and rescue (SAR). The MH-60S has no offensive sensors but can carry the ALQ-144 Infrared Jammer. The MH-60S will, in the near future, deploy with the AQS-20A Mine Detection System and an Airborne Laser Mine Detection System (ALMDS) for identifying submerged objects in coastal waters. The S-model is the first US Navy helicopter to field the glass cockpit whereby the flight data information is relayed to pilots using four digital screens rather than electromechanical gauges and dials. The primary means of defense is with the M60D, M240 or GAU-17/A machine guns. A \"batwing\" refit (Armed Helo Kit) based on the Army\'s UH-60L was developed to accommodate Hellfire, Hydra 70 2.75 inch rockets, or larger guns or cannons.

The MH-60S is unofficially known as the \"Knighthawk\", reflecting its role as the designated successor of the Sea Knight, though this name was formally disapproved in favor of the \"Seahawk\" name. A standard crew for the \"Knighthawk\" is one pilot, one copilot and two others depending on mission. With the retirement of the Sea Knight, the squadron designation of Helicopter Combat Support Squadron (HC) was also retired from the Navy. Operating MH-60S squadrons were re-designated Helicopter Sea Combat (HSC).

MH-60R Seahawk

The MH-60R was originally referred to as \"LAMPS Mark III Block II Upgrade\" when it began development in 1993. Two SH-60Bs were converted by Sikorsky for the project. The first modified SH-60 made its maiden flight on 22 December 1999. These conversions, designated YSH-60R, were delivered to NAS Patuxent River in 2001 for flight testing. The production variant was redesignated MH-60R to match its multi-mission capability.

The MH-60R is designed to combine the features of the SH-60B and SH-60F. Its sensors include the ASE package, MTS-FLIR, an advanced airborne fleet data link, and a more advanced airborne active sonar. It does not carry the MAD suite. Pilot instrumentation will be based on the MH-60S\'s glass cockpit, using several digital monitors instead of the complex array of dials and gauges in Bravo and Foxtrot aircraft. Offensive capabilities are improved by the addition of new Mk-54 air-launched torpedoes and Hellfire missiles. All Helicopter Anti-Submarine (HS) and Helicopter Anti-Submarine Light (HSL) squadrons that receive the Romeo will be redesignated Helicopter Maritime Strike (HSM) squadrons.

Gallery Images

Sikorsky SH-60B Seahawk


Crew : Three, consisting of a pilot, copilot and a sensor operator
Country of Origin : USA


Number Of Engines : Two
Powerplant type : General Electric T700-GE-401 turboshaft engine
Max Power Rating : 1,260kW (1,690shp)


Length, Rotors Turning : 19.76m (64ft 10in)
Length, Rotors And Tail Folded : 12.47m (40ft 11in)
Height, Rotors Turning : 5.18m (17ft)
Tailplane Span : 4.38m (15ft 10in)
Main Rotor Diameter : 16.36m (53ft 8in)
Main Rotor Disc Area : 210.14m2 (2,262sq ft)
Tail Rotor Diameter : 3.35m (11ft)


Empty Weight : 6,191kg (13,648lb)
Internal fuel load : 1,089kg (2,400lb)

Landing Gear

Type : Fixed tailwheel type with single-wheel main units and a twin-wheel tail unit
Wheelbase : 4.83m (15ft 10in)
Wheel Track : 2.79m (9ft 2in)


Service Ceiling : 19,000ft (5,790m)

Sikorsky UH-60A Blackhawk


Crew : Three
Country of Origin : USA
Accommodation : Up to 11 troops


Number Of Engines : Two
Powerplant type : General Electric T700-GE-700 turboshafts
Max Power Rating : 1,163kW (1,560shp)


Length, Rotors Turning : 19.76m (64ft 10in)
Length, Rotors And Tail Folded : 12.60m (41ft 4in)
Height, Rotors Turning : 5.13m (16ft 10in)
Tailplane Span : 4.38m (14ft 4.5in)
Main Rotor Diameter : 16.36m (53ft 8in)
Main Rotor Disc Area : 210.05m2 (2,261sq ft)
Tail Rotor Diameter : 3.35m (11ft)


Empty Weight : 4,819kg (10,624lb)
Max Take-off Weight : 9,185kg (20,250lb)
Internal fuel load : 1,340 litres (354 US gal)

Landing Gear

Type : Fixed tailwheel type with a single wheel on each unit
Wheelbase : 8.83m (28ft 11.75in)
Wheel Track : 2.71m (8ft 10.5in)


Max Speed At Sea Level : 160kt (296km/h; 184mph)

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