SIKORSKY (S-70B) SH-60 SEAHAWK
US Navy designation: SH-60B and SH-60R Seahawk, SH-60F and HH-60H
US Coast Guard designation: HH-60J Jayhawk
Japanese Maritime Self-Defence Force designation: SH-60J
Spanish Navy designation: HS.23
Taiwanese Navy designation: S-70C(M)-1 and S-70C(M)-2 Thunderhawk
TYPE:
- ASW/Anti-Ship Surveillance and Targeting (ASST)/SAR helicopter.
PROGRAMME:
- The Kaman SH-2 was considered to be unsuitable for the new LAMPs systems. In 1977, year after S-70A had been selected for the Army, the Navy conducted a similar evaluation.
- The YUH-60A Sikorsky airframe was selected for the new LAMPS Mk III (Light Airborne Multi-Purpose System).
- First flight of YSH-60B on December 12, 1979.
- Two years of development and testing before initial production.
- First flight of production aircraft on February 11, 1983.
- Changed USN planning in 1993 resulted in premature end to SH-60B/F production.
- SH-60F to be withdrawn from aircraft carriers and remanufacture all SH-60B/Fs as SH-60R.
VARIANTS:
SH-60B
- Initial production version for ASW/ASST.
SH-60F Ocean Hawk
- CV Inner Zone ASW helicopter.
- Known as CV-Helo, for close-in ASW protection of aircraft carrier groups to replace SH-3H Sea King.
- First flight of SH-60F on March 19, 1987.
- Production terminated with final delivery on December 1, 1994.
- To be phased out of carrier operations and conversions to SH-60R planned, thought some may become HH-60Hs.
- The SH-60F configuration has all LAMPS Mk III avionics, fairings and equipment removed, including cargo hook and RAST system main and tail probes.
- Features include:
- Integrated ASW mission avionics including AlliedSignal AN/AQS-13F dipping sonar.
- MIL-STD-1553B databus.
- Dual Teledyne Systems AN/ASN-150 tactical navigation computers.
- AN/ASM-614 avionics support equipment.
- Automatic flight control system with quick automatic transition and both cable and Doppler autohover.
- Tactical datalink with other aircraft.
- Communications control system.
- Multifunction keypads and displays for each of four crew members.
- Internal/external fuel system and extra weapon station to port allowing carriage of three Mk 50 homing torpedoes.
- Provision for surface search radar.
- FLIR, night vision equipment.
- Passive ECM, MAD, air-to-surface missile capability.
- Sonobuoy datalink.
- Chaff/sonobuoy dispenser.
- Attitude and heading reference system (AHRS), Navstar GPS.
- Fatigue monitoring system.
- Increase of maximum T-O weight to 10,659 kg (23,500 lb).
HH-60H
- A strike-rescue/special warfare support (HCS) variant.
- Designated HH-60H in September 1986.
- First flight on August 17, 1988.
- Accepted by USN on March 30, 1989.
- Missions requirements are to recover four-man crew at 250 n miles (463 km, 288 miles) from launch point or fly 200 n miles (371 km, 230 miles) and drop eight SEALs from 915 m (3,000 ft).
- A close derivative of SH-60F with same T700-GE-401C engines and HIRSS as SH-60B/F.
- Equipment includes:
- General Instrument AN/APR-39A(XE)2 RWR.
- Hughes AN/AVR-2 laser warning receiver.
- Honeywell AN/AAR-47 missile plume detector.
- Lockheed Martin AN/ALE-47 chaff/flare dispenser.
- Sanders AN/ALQ-144 IR jammer.
- Elbit ANVIS 7 NVG/HUD system.
- Two cabin-mounted M60D 7.62 mm machine guns.
- Provision for weapon pylons.
- Cubic AN/ARS-6 personnel locator system installed from FY91.
- Some equipped with Seahawk-type Indal RAST (recovery assist, secure and traverse) equipment.
HH-60J Jayhawk
- Ordered in parallel with HH-60H, adapted for US Coast Guard medium-range recovery (MRR) role.
- First flight on August 8, 1989.
- When carrying three 455 litre (120 US gallon, 100 Imp gallon) external tanks, HH-60J can fly out 300 n miles (556 km, 345 miles) and return with six survivors in addition to four-man crew or loiter for 1 hour 30 minutes when investing possible smuggles.
- Other duties include law enforcement, drug interdiction, logistics, aids to navigation, environmental protection and military readiness.
Equipment includes:
- AlliedSignal RDR-1300C search/weather radar.
- AN/ARN-147 VOR/ILS.
- KDF 806 direction-finder.
- GPS, Tacan, VHF/UHF-DF, TacNav.
- Dual U/VHF-FM radios, HF radio.
- ILL/V/U/HF IFF crypto computers.
- NVG-compatible cockpit.
- Rescue hoist and external cargo hook.
XSH-60J
- Japanese Maritime Self-Defence Force (JMSDF) placed an order for two S-70B-3s for installation of Japanese avionics and mission equipment.
- First flights on August 31 and early October 1987.
- Includes Japanese avionics but the AN/APS-124 radar.
SH-60J
- Mitsubihi is manufacturing SH-60J Seahawk for JMSDF to replace Sikorsky SH-3 Sea King.
UH-60J/UH-60JA
- Japanese variants of Black Hawk.
SH-60R
- Remanufactured Seahawk.
- Combines SH-60B capabilities with dipping sonar of Sh-60F.
- US Navy planned 273 existing SH-60Bs, SH-60Fs and HH-60Hs to be converted.
- Sh-60R systems to be orientated towards littoral warfare operations, with ability to process and prosecute large number of air and sea contacts in a comparatively confined space.
- New system to enhance countermeasures and passive and active detection capability will be added.
- These include:
- Telephonics AN/APS-147 multitone radar.
- Raytheon AN/AAS-44 FLIR/laser ranger.
- AN/AYK-14 and AN/UYS-2 processors.
- Colour high-resolution displays.
- Dual INS with GPS.
- Air-air and air-ship datalinks.
- Satellite communications.
- Lockheed Martin ESM system with expanded detection frequency band.
- Laser detector.
- MIL-STD-1760 stores stations.
- Hughes/Thompson-CSF AN/AQS-22 airborne low-frequency sonar.
- New keyseats and displays will also be installed, with an upgraded Hamilton Standard flight control computer.
- SH-60B's MAD and floatation device to be deleted.
- Hellfire ASM and SH-60B weapons included.
- Service Life Extension Programme (SELP) to be included in the upgrade process as some SH-60Bs are nearing the projected life of 10,000 hours.
S-70B-1
- Spanish Navy received six from December 1988 and designated HS.23.
- Similar to USN SH-60B but with AlliedSignal AN/AQS-13F dipping sonar.
S-70B-2
- Royal Australian Navy selected the Seahawk for role adaptable weapon system (RAWS) full-spectrum ASW helicopter with autonomous operating capability.
- First flight on December 4, 1987.
- S-70B-2 has different avionics than the USN version, such as:
- Thomson Thorn Super Searcher radar.
- Collins advanced integrated avionics including cockpit controls and displays.
- Navigation receivers.
- Communications radios.
- Airborne target handoff datalink and tactical data system (TDS).
S-70B-6
- Hybrid SH-60B/F for Greece.
- Armament includes NFT Penguin ASMs.
- Avionics include AN/AQS-18(V)-3 dipping sonar, AN/APS-14(V)-3 radar and AN/ALR-66(V)-2 ESM.
S-70B-28
- Ordered for Turkish Navy on February 14, 1997.
- Armament include the use of AGM-114 Hellfire ASM.
S-70C(M)-1/2 Thunderhawk
- Delivery began in July 1990 to Taiwanese Navy.
- Equipment includes:
- AlliedSignal AN/AQS-18(V) dipping sonar.
- Telephonics AN/APS-128PC radar.
- Litton AN/ALR-606(V)-2 ESM integrated with radar antenna.
- Large antenna array positioned on top of main rotor assembly.
- Sigint system used to intercept HF and VHF radio communications.
Following descriptions applies to SH-60B
DESIGN FEATURES
- Seahawk designed to provide all-weather detection, classification, localization, and interdiction of surface ships and submarines, either controlled through datalink from mother ship or operated independently.
- Secondary mission include SAR, vertical replenishment, medevac, fleet support and communications relay.
- Structure is basically same as UH-60 plus marine corrosion protection, single cabin door narrower than the UH-60's.
- New features include:
- More powerful navalized GE-T700-GE-401 engines, additional fuel.
- Sensor operator's station.
- Port-side internal launchers for 25 sonobuoys.
- Pylons on starboard side of tailboom for MAD bird.
- Lateral pylons for two torpedoes for external tanks.
- Chin-mounted ESM pods.
- Sliding cabin door.
- Rescue hoist.
- Electrically actuated blade folding.
- Rotor brake.
- Folding tail.
- Short-wheelbase tailwheel landing gear with twin tailwheels stressed for lower crash impact.
- DAF Indal RAST recovery assist.
- Secure and traversing for haul-down landings on small decks and moving into hanger.
- Hovering in-flight refuelling system.
- And emergency floatation system.
- During the Gulf War, 25 SH-60Bs were fitted with upper and lower Sanders AN/ALQ-144 IR jammers, Tracor AN/ALE-39 chaff/flare dispensers, Honeywell AN/AAR-7 electro-optical missile warning, and a single 7.62 mm machine gun in door.
POWER PLANT:
- Two 1,260 kM (1,690 shp) intermediate rating general Electric (T700-GE-401 turboshafts in early aircraft.
- 1,342 kM (1,800 shp) T700-GE-401C turboshafts introduced in 1988 and on HH-60H/J.
- Transmission rating of 2,535 kW (3,400 shp).
- Internal fuel capacity: 2,233 litres (590 US gallons, 491 Imp gallons).
- Hovering in-flight refuelling capability.
- Two 455 litre (120 US gallon, 100 Imp gallon) auxiliary fuel tanks on fuselage pylons (three on HH-60J).
- Hover IR suppressor subsystem (HIRSS) exhaust cowling fitted on HH-60H.
ARMAMENT:
- US Navy armament includes two Mk 46 torpedoes, NFT AGM-119B Penguin Mk 2 Mod 7 anti-ship missiles, and Honeywell Mk 50 Advanced Lightweight Torpedoe.
- HH-60H has two pintle-mounted M60D machine guns.
- Cleared in 1996 to operated Rockwell AGM-114 Hellfire ASM on SH-60B/R.
- HH-60H also to receive 70 mm (2.75 in) rocket pods and forward-firing guns.
| DIMENSIONS: (SH-60B, otherwise indicated) |
| Length overall, rotors and tail pylon folded: | | |
| SH-60B: | 12.47 m | 40 ft 11 in |
| HH-60H: | 12.51 m | 41 ft 5/8 in |
| HH-60J: | 12.13 m | 43 ft 7/8 in |
| Length, rotors turning (SH-60B): | 19.76 m | 64 ft 10 in |
| Length of fuselage: | | |
| SH-60B: | 15.3 m | 50 ft |
| HH-60J: | 15.87 m | 52 ft 1 in |
| Rotor Diameter: | 16.4 m | 53 ft 8 in |
| Height: | | |
| Overall, tail rotor turning: | 5.18 m | 17 ft 0 in |
| Overall, pylon folded: | 4.04 m | 13 ft 3 ¼ in |
| To top of rotor head: | 3.79 m | 12 ft 5 3/8 in |
| Main rotor disc area: | 210.14 m2 | 2,262.04 sq ft |
| WEIGHTS AND LOADINGS: |
| Weight empty: | | |
| SH-60B: | 6,191 kg | 13,648 lb |
| HH-60H: | 6,114 kg | 13,480 lb |
| HH-60J: | 6,086 kg | 13,417 lb |
| Mission gross weight: | | |
| SH-60B ASW: | 9,182 kg | 20,244 lb |
| SH-60B ASST: | 8,334 kg | 18,373 lb |
| Max T-O weight: | | |
| SH-60B/HH-60H: | 9,926 kg | 21,884 lb |
| HH-60J: | 9,637 kg | 21,246 lb |
| Payload: | 3,551 kg | 7,829 lb |
| PERFORMANCE: |
| Cruising speed at S/L: | | |
| SH-60B/HH-60H: | 147 kt | 272 km/h, 169 mph |
| HH-60J: | 146 kt | 271 km/h, 168 mph |
| Vertical rate of climb at S/L: | 213 m/min | 700 ft/min |
| Range: | 319 n miles | 592 km, 368 miles |
| Combat radius with 3h loiter in patrol area: | 92.5 km | 57.5 miles |