鐵之狂傲

標題: 『每日軍事武器鑑賞』－ UH-60 『黑鷹』多用途直升機 [列印本頁]

作者: 克里斯Chris 時間: 07-4-27 18:22
標題: 『每日軍事武器鑑賞』－ UH-60 『黑鷹』多用途直升機
UH-60 Black Hawk

The Black Hawk is the Army旧 front-line utility helicopter used for air assault, air cavalry, and aeromedical evacuation units. It is designed to carry 11 combat-loaded, air assault troops, and it is capable of moving a 105-millimeter howitzer and 30 rounds of ammunition. First deployed in 1978, the Black Hawk旧 advanced technology makes it easy to maintain in the field. The Black Hawk has performed admirably in a variety of missions, including air assault, air cavalry and aeromedical evacuations. In addition, modified Black Hawks operate as command and control, electronic warfare, and special operations platforms.

The UH-60A, first flown in October 1974, was developed as result of the Utility Tactical Transport Aircraft System (UTTAS) program. The UTTAS was designed for troop transport, command and control, MedEvac, and reconnaissance, to replace the UH-1 Series "Huey" in the combat assault role. In August 1972, the U.S. Army selected the Sikorsky (model S-70) YUH-60A and the Boeing Vertol (model 237) YUH-61A (1974) as competitors in the Utility Tactical Transport Aircraft System (UTTAS) program. The Boeing Vertol YUH-61A had a four-bladed composite rotor, was powered by the same General Electric T700 engine as the Sikorsky YUH-60A, and could carry 11 troops. In December 1976 Sikorsky won the competition to produce the UH-60A, subsequently named the Black Hawk.
The Black Hawk is the primary division-level transport helicopter, providing dramatic improvements in troop capacity and cargo lift capability compared to the UH-1 Series "Huey" it replaces. The UH-60A, with a crew of three, can lift an entire 11-man fully-equipped infantry squad in most weather conditions. It can be configured to carry four litters, by removing eight troop seats, in the MedEval role. Both the pilot and co-pilot are provided with armor-protective seats. Protective armor on the Black Hawk can withstand hits from 23mm shells. The Black Hawk has a cargo hook for external lift missions. The Black Hawk has provisions for door mounting of two M60D 7.62mm machine guns on the M144 armament subsystem, and can disperse chaff and infrared jamming flares using the M130 general purpose dispenser. The Black Hawk has a composite titanium and fiberglass four-bladed main rotor, is powered by two General Electric T700-GE-700 1622 shp turboshaft engines, and has a speed of 163 mph (142 knots).

Elements of the US Army Aviation UH-60A/l Blackhawk helicopter fleet will begin reaching their sevice life goal of 25 years in 2002. In order for the fleet to remain operationally effective through the time period 2025-2030 the aircraft will need to go through an inspection, refurbishment, and modernization process that will validate the structural integrity of the airframe, incorporate improvements in sub-systems so as to reduce maintenance requirements, and modernize the mission equipment and avionics to the levels compatible with Force XXI and Army After Next (AAN) demands.

A Service Life Extension Program (SLEP) is planned for the UH-60 beginning in FY99. The UH-60 modernization program will identify material requirements to effectively address known operational deficiencies to ensure the Black Hawk is equipped and capable of meeting battlefield requirements through the 2025-2030 timeframe. Primary modernization areas for consideration are: increased lift, advanced avionics (digital communications and navigation suites), enhanced aircraft survivability equipment (ASE), increased reliability and maintainability (R & M), airframe service life extension (SLEP), and reduced operations and support (O & S) costs. Suspense date for the approved Operational Requirements Document (ORD) is December 1998.

作者: 克里斯Chris 時間: 07-4-27 18:22
Variants
The Army began fielding the UH-60 in 1978. From 1978 until 1989 the Army procured UH-60A model aircraft. In October 1989, a power train upgrade resulted in a model designation change from UH-60A to UH-60L. The UH-60L version that provides 24 percent more power than the original 1970 UH-60A model. As of the end of FY97, the Army had procured 483 UH-60L models for a total UH-60 acquisition of 1,463 aircraft. The Army is in the fifth and final year of a multi-year procurement contract calling for the delivery of 60 aircraft per year.

UH-60L
In October 1989, the engines were upgraded to two General Electric T700-GE-701C 1890 shp turboshaft engines, and an improved durability gear box was added, resulting in a model designation change from UH-60A to UH-60L. The T700-GE-701C has better high altitude and hot weather performance, greater lifting capacity, and improved corrosion protection. The helicopter can carry a gross weight of 22,000 Lbs and an external load of 9,000 Lbs. The UH-60L variant can utilize an External Stores Support System or ESSS to expand its capabilities. The ESSS system consists of removable "four-station pylons" that can carry external fuel tanks that can extend the Blackhawk range up to 1,150 nautical miles or sixteen Hellfire missiles. Furthermore, Sikorsky states that the Blackhawk can store an additional sixteen Hellfire missiles internally, and deploy a wide range of weapons systmes ranging from guns to mine dispensers.

作者: 克里斯Chris 時間: 07-4-27 18:23

Specifications
Manufacturer	Sikorsky Aircraft
Performance	Max Cruise Speed
	4,000 ft; 95°F 152 knots
	2,000 ft; 70°F 159 knots
	SLS 155 knots
	VNE 193 knots
Vertical rate of Climb	95% MRP
	4,000 ft; 95°F 1,550 ft per minute
	2,000 ft; 70°F 2,750 ft per minute
	SLS > 3,000 ft per minute
Service Ceiling	(ISA day) 19,1510 ft
	Hover Ceiling MRP-OGE
	95°F 7,650 ft
	70°F 9,375 ft
	Standard Day 11,125 ft
Weight	Empty 11,516 Lbs
	Mission gross weight - 17,432 Lbs
	Maximum gross weight - 22,000 Lbs
	Maximum gross weight (ferry) - 24,500 Lbs
Length	64 ft 10 in
Height	16 ft 10 in
Rotor	Diameter 53 ft 8 in
	Four titanium and fiberglass blades

作者: 克里斯Chris 時間: 07-4-27 18:23
UH-60 Firehawk
is a Reseach and Development program to provide the UH-60 series helicopter with both a wartime and peacetime fire fighting capability by use of a detachable 1,000 gal. belly tank. Qualification issues include design and testing required to maintain the combat capabilities of the UH-60 Black Hawk and the safe flight envelope of the aircraft with the tank.

EH-60A
Electronic Countermeasures (ECM) variant has a unique external antenna designed to intercept and jam enemy communications. The EH-60E is powered by two General Electric T700-GE-700 1622 shp turboshaft engines.

EH-60B
version was a Stand-Off Target Acquisition System designed to detect the movement of enemy forces on the battlefield and relay the information to a ground station.

作者: 克里斯Chris 時間: 07-4-27 18:23
UH-60Q MEDEVAC

The UH-60Q MEDEVAC helicopter provides significant enroute patient care enhancements. The UH-60Q provides a 6 patient litter system, on-board oxygen generation, and a medical suction system. UH-60Q is a UH-60A derivative and incorporates approximate UH-60A characteristics. It is simply the best in aeromedical evacuation. Building on the BLACK HAWK's heritage of saving lives in Grenada, Panama, Kuwait and Somalia, the UH-60Q delivers exceptional patient care, increased survivability, longer range, greater speed and added missions capability. For military combatants. War victims. Civilians injured in natural disasters. It has a state-of-the-art medical interior that can accomodate a crew of three and up to six acute care patients. The UH-60Q's leading-edge technology incorporates an improved environmental control system. Cardiac monitoring systems. Oxygen generation, distribution and suction systems. Airway management capability. Provision for stowing IV solutions. And an external electrical rescue hoist. And in addition to extensive immediate care, the UH-60Q can perform all weather terrain battlefield evacuation, combat search and rescue, hospital ship lifeline missions, deep operations support, forward surgical team transport, medical logistics resupply, medical personnel movement, patient regulating, disaster/humanitarian relief, and MAST/HELP state support.

The UH-60Q's medical interior can accomodate three to six acute care patients and their medical attendants. Ergonomic design has maximized the UH-60Q cabin space, placing sophisticated, life-saving instruments and equipment at the fingertips of the medical attendants. A unique platform design allows the interior to transport either six litter of seven ambulatory systems, oxygen distribution and suction systems, airway management capability, and provisions for stowing intravenous solutions. The interior also features these additional capabilities, essentical to providing the highest degree of patient care when every second counts:
Oxygen Generating Systems
NVG Compatible Lighting Throughout
Environmental Control System
Medical Equipment
Patient Monitoring Equipment
Neonatal Isolettes

The UH-60Q communications architecture provides situational awareness and digital communications and is expected to be the model for anticipated fleet-wide improvements to the UH-60. Other improvements include integrated Doppler/GPS, Personnel Locator System, NVG interior lighting, and FLIR.
Modernizing the Medical Evacuation (MEDEVAC) system is the Army Surgeon General's number one near term priority. The General Accounting Office identified the evacuation deficiency in its report to Congress in 1992. The Army Plan states, "Enhance the battlefield medical system by acquiring modern medical evacuation aircraft" Lessons learned from Operations Just Cause and Desert Storm showed a need for medical version of the UH-60. The UH-60Q was a TRADOC FY96-10 and FY97-11 "must have" Warfighting Lens Analysis solution in order to decrease risk, improve deployability, supportability and training of the force and ensure survivability of Early Entry/Dismounted Forces. Medical Evacuation was the Surgeon General旧 number one near-term medical modernization priority in the FY94-08, FY95-09, &FY96-10 Army Modernization Plan. CINC requests the replacement of UH-1 MEDEVAC aircraft with UH-60Q.

作者: 克里斯Chris 時間: 07-4-27 18:24

Specifications
Manufacturer	Sikorsky Aircraft
Length	64 feet 10 inches(rotor turning)
Width	53 feet 8 inches (rotor turning)
Height	16 feet 10 inches (overall)
Weight	11,500 pounds
Propulsion	Two T700-GE-701Cs
Crew	Three
Speed	150 knots
Vertical Rate of Climb	185 FPM
Max Range	315 nm (internal fuel)

作者: 克里斯Chris 時間: 07-4-27 18:24
MH-60G Pave Hawk
The Pave Hawk is a twin-engine medium-lift helicopter operated by the Air Force Special Operations Command, a component of the U.S. Special Operations Command. The MH-60G's primary wartime missions are infiltration, exfiltration and resupply of special operations forces in day, night or marginal weather conditions. Other missions include combat search and rescue. During Desert Storm, Pave Hawks provided combat recovery for coalition air forces in Iraq, Saudi Arabia, Kuwait and the Persian Gulf. They also provided emergency evacuation coverage for U.S. Navy sea, air and land (SEAL) teams penetrating the Kuwait coas t before the invasion.

The MH-60G is equipped with an all-weather radar which enables the crew to avoid inclement weather. To extend their range, Pave Hawks are equipped with a retractable in-flight refueling probe and internal auxiliary fuel tanks. Pave Hawks are equipped with a rescue hoist with a 200-foot (60.7 meters) cable and 600-pound (270 kilograms) lift capacity. All MH-60G's have an automatic flight control system to stabilize the aircraft in typical flight altitudes. They also have instrumentation and engine and rotor blade anti-ice systems for all-weather operation. The non-retractable landing gear consists of two main landing gears and a tail wheel. Aft sliding doors on each side of the troop and cargo compartment allow rapid loading and unloading. External loads can be carried on an 8,000-pound (3,600 kilograms) capacity cargo hook. Pave Hawks are equipped with folding rotor blades and a tail stabilator for shipboard operations and to ease air transportability.

MH-60K is the standard special operations version of the Black Hawk. It is capable of providing long-range airlifts far into hostile territory in adverse weather conditions. Modifications include two removable 230 gallon external fuel tanks, two .50 cal. machine guns, an air-to-air refueling probe, and an external hoist. The MH-60K can also be armed with two M134 7.62mm "miniguns". A new avionics suite includes interactive Multi-Function Displays (MFDs), Forward-Looking Infrared (FLIR), digital map generator, and terrain avoidance/terrain following multi-mode radar. Survivability equipment includes radar and missile warning systems and IR jammers. The MH-60K has full shipboard operability. It is powered by two General Electric T700-GE-701C 1843 shp turboshaft engines.

The older MH-60L can be adapted to the attack mission by attaching dual weapons pylons to both sides of the fuselage. Pylon mounting cannon, rockets, or missiles can be supplemented by door or port mounting guns or launchers, limited mainly by the range, duration, cargo, or troops required to complete the mission. The helicopter's mission is insertion and extraction of special operations troops. Survivability equipment includes radar and missile warning systems and IR jammers. The MH-60L is powered by two General Electric T700-GE-701C 1843 shp turboshaft engines.

作者: 克里斯Chris 時間: 07-4-27 18:24

Specifications
Primary Function	Infiltration, exfiltration and resupply of special operations forces in day, night or marginal weather conditions.
Builder	Sikorsky Aircraft Corp.
Power Plant	Two General Electric T700-GE-01C engines
Thrust	1,630 shaft horsepower, each engine
Length	64 feet, 8 inches (17.1 meters)
Height	16 feet, 8 inches (4.4 meters)
Rotary Diameter	53 feet, 7 inches (14.1 meters)
Speed	184 mph (294.4 kph)
Maximum Takeoff Weight	22,000 pounds (9,900 kilograms)
Range	445 nautical miles; 504 statute miles (unlimited with air refueling)
Armament	Two 7.62mm mini-guns
Costs	$10.1 million (1992 dollars) Unit Cost
Crew	Two pilots, one flight engineer and one gunner
Date Deployed	1982
Inventory	Active force, 10; ANG, 0; Reserve, 0

作者: 克里斯Chris 時間: 07-4-27 18:25
HH-60G Pave Hawk

The HH-60G's primary wartime mission is combat search and rescue, infiltration, exfiltration and resupply of special operations forces in day, night or marginal weather conditions. The HH-60G Pave Hawk provides the capability of independent rescue operations in combat areas up to and including medium-threat environments. Recoveries are made by landing or by alternate means, such as rope ladder or hoist. Low-level tactical flight profiles are used to avoid threats. Night Vision Goggle (NVG) and Forward Looking Infrared (FLIR) assisted low-level night operations and night water operation missions are performed by specially trained crews. The basic crew normally consists of five: pilot, co-pilot, flight engineer, and two PJs. The aircraft can also carry eight to 10 troops.
Pave Hawks are equipped with a rescue hoist with a 200-foot (60.7 meters) cable and 600-pound (270 kilograms) lift capacity. The helicopter hoist can recover survivors from a hover height of 200 feet above the ground or vertical landings can be accomplished into unprepared areas. The hoist can recover a Stokes litter patient or three people simultaneously on a forest penetrator.

The helicopter has limited self-protection provided by side window mounted M-60, M-240, or GAU-2B machine guns. Pave Hawk is equipped with two crew-served 7.62mm miniguns mounted in the cabin windows. Also, two .50 caliber machine guns can be mounted in the cabin doors. An APR-39A(V)1 radar warning receiver, ALQ-144A infrared jammer, Hover Infrared Suppression System (HIRSS), M-130 chaff dispenser, and precision navigation equipment (GPS, Inertial Navigation System (INS), Doppler) afford additional threat avoidance and protection.

Mission systems on the HH-60H make it ideally suited for operations with special warfare units. Combat-equipped personnel can be covertly inserted and/or extracted in any terrain with precise GPS navigation accuracy. A variety of insertion and extraction techniques are available, including landing, hoisting, fastrope, rappel, paradrop, McGuire or SPIE Rig, and CRRC. Additionally, Helicopter Visit Board Search and Seizure (HVBSS) operations may be conducted using one or more of these insertion/extraction techniques. HVBSS missions are designed to take control of a ship considered to be a Contact of Interest (COI). The ability to interdict or 'take down' shipping during enforcement of a naval blockade requires precise planning and execution. Tethered Duck (T-Duck) was implemented to rapidly insert troops and a Combat Rubber Raiding Craft (CRRC) to water areas. The troops fastrope down to the CRRC after it is lowered into the water, and the motor is then hoisted down to the troops to complete the procedure. Parachute operations are used for inserting troops when the helicopters are unable to land with a minumum free-fall drop altitude of 2500 feet AGL (above ground level).

The maximum speed is 193 knots with a cruise speed of 120 to 140 knots. Unrefueled range is 480 nautical miles (NM), with a combat load and aircraft at maximum gross weight of 22,000 lbs; the combat radius is approximately 200NM. Inflight refueling greatly extends this range. Pave Hawks are equipped with a retractable in-flight refueling probe and internal auxiliary fuel tanks.
All HH-60G's have an automatic flight control system to stabilize the aircraft in typical flight altitudes. They also have instrumentation and engine and rotor blade anti-ice systems for all-weather operation. The HH-60G is equipped with an all-weather radar which enables the crew to avoid inclement weather. Pave Hawks are equipped with folding rotor blades and a tail stabilator for shipboard operations and to ease air transportability. The non-retractable landing gear consists of two main landing gears and a tail wheel. Aft sliding doors on each side of the troop and cargo compartment allow rapid loading and unloading. External loads can be carried on an 8,000-pound (3,600 kilograms) capacity cargo hook. The Pave Hawk can be equipped with the external stores support system.

The HH-60 is stationed throughout the world. MAJCOMS include AFRC, ANG, AFSOC, PACAF, AFMC, AETC, and ACC. ACC is the lead command. Besides a full complement of flightline support, home stations provide two and three level maintenance support functions. HH-60 helicopter is a worldwide deployable aircraft. Two 365 day a year contingencies are currently being conducted. In deployment scenarios some locations have full flightline support capabilities with limited backshop support, while other deployed sites have less support, down to a bare base scenario. A flightline support contingent is deployed with the aircraft. Depending on the deployment location and duration, varying levels of backshop maintenance support might also be deployed.

HH-60G is rapidly approaching its flying hour service life limit. Consequently, CAF will soon require either a service life extension program (SLEP) for HH-60G or procurement of a replacement aircraft for conducting CSAR operations. The HH-60G System Program Office (WR-ALC/LU) is assessing whether HH-60G旧 service life limit is 8,000 flight hours, IAW the Army specification for the H-60 airframe, or actually closer to 7,000 flight hours based upon AF configuration and operating gross weights of the HH-60G. Depending on the assessment results, HH-60G aircraft (1981 models) will begin reaching their service life limit as early as FY00, if service life limit is determined to be 7,000 flight hours. Otherwise, if the limit is determined to be 8,000 flight hours, 1981 model HH-60G aircraft will begin reaching their service life limit in FY03.

作者: 克里斯Chris 時間: 07-4-27 18:26

Air Combat Command (ACC) is analyzing concepts/alternatives to assess their relative cost effectiveness and affordability for sustaining the U.S. Air Force's Combat Search and Rescue (CSAR) capability. After complete concepts/alternatives (aircraft platform- level,including subsystems, and support/training systems) are received, the Air Force intends to analyze those that provide the most opportunity to satisfy currently deficient mission capabilities while maintaining, as a minimum, existent Combat Rescue capability. A detailed Analysis of Alternatives (AoA) will follow to ascertain whether or not the concepts/alternatives exceed/meet/do not meet the specific measures of effectiveness. The AoA will include modeling, simulation, and CSAR scenarios projected for 2010. If this analysis results in the initiation of an acquisition program to procure a replacement for the HH-60G aircraft, the Initial Operational Capability (IOC) would be in place by the end of FY07.
CSAR - Combat Rescue Analysis of Alternatives PIXS - Preaward Information eXchange System
CSAR - Combat Rescue Analysis of Alternatives Industry Day - 17 November 1999
AoA Backgound
AoA Mission Description
CSAR Baseline Performance
CSAR Operations and Support
Combat Rescue Mission Needs & Deficiencies
AoA Overview
AoA Analysis

作者: 克里斯Chris 時間: 07-4-27 18:26
CH-60 Sea Hawk
The current Fleet Combat Support Helicopter provides the Navy's Combat Logistics Force (CLF) with an at-sea Vertical Replenishment (VERTREP) capability. It also serves as the primary Search and Rescue (SAR) helicopter for the Amphibious Task Force (ATF), providing essential support to amphibious operations. The primary missions of the CH-60 will include day and night VERTREP, day and night amphibious SAR, vertical onboard delivery, and airhead operations. Secondary missions of the CH-60 will include Combat Search and Rescue (CSAR), Special Warfare Support (SWS), recovery of torpedoes, drones, unmanned aerial vehicles, and unmanned undersea vehicles, noncombatant evacuation operations, aeromedical evacuations, humanitarian assistance, executive transport, and disaster relief. The CSAR/SWS version of the CH-60 will have additional mission equipment installed that will provide the Navy with capabilities for CSAR and SWS in both the active carrier-based Helicopter Antisubmarine Squadrons (HS) and in the Reserve Helicopter Combat Support (Special) (HCS) Squadrons.

Based on the current deployment schedule, the CH-60 will first replace the H-46D helicopters in active Navy Helicopter Combat Support (HC) Squadrons. After the H-46s have been replaced, the CH-60 will replace the HH-60H helicopters in the Reserve HCS squadrons, then the UH-3H and HH-1H helicopters used as Naval Air Station SAR, range support, and executive transport missions. Finally, the CH-60 will replace the HH-60H helicopters in active Navy HS squadrons.
The CH-60 configuration evolved to fill the Navy旧 need for a comprehensive, rugged utility helicopter to replace the helicopters engaged in vertical replenishment (CH-46D, UH-46D and HH-46D), amphibious assault ship search and rescue (HH-46D), strike rescue and special warfare (HH-60H), station search and rescue (HH-1N and UH-3H), utility transport and target recovery (UH-3H), and VIP transport (VH-3A and UH-3H). The CH-60 will also be capable of carrying FLIR and Hellfire missiles, making it an even more versatile platform. The Navy needed a Seahawk variant but could not afford a utility version. Since the Army Black Hawk was much less expensive, the solution was to build a hybrid铘嘆avalized?Black Hawk that would meet the cost constraints but could be modified to operate in a ship-board environment. This takes advantage of the existing H-60 support infrastructure and reduces the number of different types of aircraft in the inventory. The Navy will save an estimated $20 billion in life-cycle costs over the life of the program.

The CH-60 will be an Army UH-60 Blackhawk utility airframe in combination with Navy SH/HH-60 transmissions and dynamic components. The CH-60 will incorporate new design items that are not in use by either the UH-60 or SH/HH-60 airframe lines. The CH-60 will adapt the Naval H-60 Tail Pylon to the Blackhawk tail cone with a CH-60 unique canted bulkhead at the tail cone, tail pylon interface. This bulkhead will 単arry?the two components by providing a Naval H-60 interface on its aft face to accommodate the Naval H-60旧 fold hinges and quick disconnect mechanism; and a UH-60 interface on its forward face to accommodate the UH-60旧 tail landing gear and tail cone interface. The Blackhawk旧 tail cone flight controls will be rerouted to accommodate the Naval H-60 rapid fold tail pylon. With a large cabin, double cargo doors and external stores support system winglets, the aircraft externally resembles a Black Hawk. Most of its Seahawk features are internal: engines, rotor brake, folding tail pylon, automatic flight control system, rescue hoist and a more durable gearbox. The production version of the aircraft will be equipped with reversible floor-boards on the cabin cargo floor, and one side will be fitted with rollers to handle up to two standard four-foot-square cargo pallets.

The CH-60 will be able to operate day or night, under adverse weather conditions, including flight in light icing. The helicopter will be compatible with all current and future Aircraft Carriers, CLF, and ATF ships to include fitting inside the hangars of all CLF ships without ship alteration. The helicopter will be capable of operating over all designated ship hover areas, both day and night, and be compatible for limited operation aboard both aviation and air capable ships proportionate with a fixed fore-to-aft wheelbase of 29 feet.

Sikorsky has tooled up for CH-60 production, and configuration options and a cockpit common with the SH-60R have being engineered. The first major assemblies of the CH-60 entered production late in 1998; first deliveries occured in late 1999.

Reducing the types of helicopters in the fleet inventory to two airframes may enable the Navy to consolidate its HS and HC (helicopter combat support) squadrons. One possibility now being considered is for a carrier battle group to deploy with SH-60Rs and CH-60s on board the carrier, with other CH-60s detached to the battle group旧 logistics ship.

The CH-60 has several advantages over the HH-60H Seahawk as a strike rescue and special warfare helicopter. The Black Hawkstyle tail wheel, positioned further aft, allows for a steeper landing approach to a confined area. The CH-60旧 larger cabin will enable it to carry more troops; its two larger cargo doors will allow more rapid deployment of the rigid inflatable boats for Navy sea-air-land team members (SEALs). The CH-60 also will be more crash-worthy, and will be fitted with better self-sealing fuel tanks capable of withstanding rounds up to 7.62 mm. The external stores support system installed on the CH-60 will allow more fuel and weapons to be carried.

作者: 克里斯Chris 時間: 07-4-27 18:26
The Navy hopes that the CH-60 will be able to meet its biggest challenge閇eplacing the gigantic Sikorsky-built MH-53E Sea Dragon minesweeping helicopter. Although the CH-60 is too small to tow the heavy MH-53E minesweeping sleds, lightweight towed systems and laser imaging detection and ranging systems promise to make the CH-60 a capable mine hunter. Because it is a hybrid of the Black Hawk and the Seahawk, the CH-60 presents a quandary for Sikorsky旧 marketing strategy: what does one call the CH-60? A possibility being considered, partly in tribute to the H-46 Sea Knight that the CH-60 will replace, is Knighthawk. The Navy still has not assigned a type/model/series designation to the CH-60; the next letter available in the H-60 series is 争.?If used, the aircraft旧 official designation would be CH-60S.
VRML 3-D Model

UH-60J
VRML by Soji Yamakawa

UH-60 Blackhawk
VRML by Soji Yamakawa

作者: 克里斯Chris 時間: 07-4-27 18:27
UH-60

作者: 克里斯Chris 時間: 07-4-27 18:27
UH-60Q MEDEVAC

作者: 克里斯Chris 時間: 07-4-27 18:27
HH-60

作者: 克里斯Chris 時間: 07-4-27 18:28
MH-60

(文章來自：黑鷹系列）

作者: 克里斯Chris 時間: 07-4-27 18:29
黑鷹（Black Hawk）

（知識）

1972年，美國陸軍展開了一項名為「通用戰術運輸機系統」（UTTAS）的計劃，該計劃決定用一種飛機取代UH－1系列直升飛機用於部隊運送、指揮控制、傷員撤離以及偵察。最後決定由西科斯基公司的YUH-60A和波音公司的YUH-61A競爭該計劃的訂單。兩種飛機均於1974年首飛其中波音公司的YUH-61A旋翼為四片複合材料槳葉，使用與YUH-60A相同的發動機，可以搭乘11人。1976年12月，西科斯基公司贏得了合同，開始製造UH-60A，起名為黑鷹（Black Hawk）

長19．76米，機身寬2．36米，高5．13米，機身為半硬殼結構。由於大量採用各類樹脂和纖維等複合材料，其空重較輕。該機最大起飛重量約10噸，最高時速292公里，航程603公里。
旋翼直徑16.36米，尾槳直徑3.35米，機長（旋翼、尾槳旋轉）19.76米，（旋翼、尾樑折疊），機身長15.26米，機高（尾槳旋轉）5.18米，（至槳轂頂部）3.79米。
最大允許速度361千米/小時，最大平飛速度（海平面）293千米/小時，最大巡航速度（高度1220米，35攝氏度）268千米/小時，垂直爬升率（海平面、32.2攝氏度）3.55米/秒，實用升限5790米，懸停高度（有地效、35攝氏度）2895米，航程（最大起飛重量、最大內部燃油、30分鐘余油）600千米，續航時間2小時18分鐘。

作者: 克里斯Chris 時間: 07-4-27 18:29
黑鷹配備了兩挺挺M60D 7.62毫米機槍，必要時可進行火力支援。

黑鷹作為突擊運輸直升機在執行低飛作戰任務時，極易遭受地面火力攻擊，故該機在提高生存力方面採取了很多措施。例如，其礬身及旋翼在製造上大量使用各類防彈材料，駕駛艙和發動機的關鍵部件均設有裝甲：兩台發動機由機身隔開，相距較遠，如有一台被擊中損壞，另一台仍可繼續工作。而黑鷹的抗墜毀措施尤其值得一提，它採用的固定式抗墜毀起落架、機身下部的蜂窩狀填料，以及高效減震座椅等，據說可保證機體在30米高度以8米／秒左右速度作粗猛著地時，最終傳到乘員身上的撞擊動能已被逐級減至人體可承受的水平。同時該機的墜毀傳感器和易斷連接器可以立即切斷電氣系統，防滲漏燃油管路及自封油箱將保證墜機後不至因漏油而失火。

UH-60機身長，且低矮，使其可以裝進C-130運輸機之中運送而不比拆掉旋翼。C-141可以運送兩架，C-5可以運送5架。

裝備情況及型號演變：

黑鷹及各類變型直升機自1979年投放市場以來，目前已售出約3000架，在全球30多個國家(地區)都擁有用戶。美國陸軍自己也裝備有1600餘架。

作者: 克里斯Chris 時間: 07-4-27 18:29
S-70A
美國陸軍型號 UH-60A、UH-60C、UH-60L、UH-60M,UH-60Q,AH-60L、EH-60A、MH-60A、MH-60K,MH-60L
　　美國空軍型號 UH-60A、HH-60G、MH-60G
　　美國海軍型號 MH-60S
　　美國海軍陸戰隊型號 VH-60N
　　以色列國防軍型號貓頭鷹(Yanshuf)
　　日本自衛隊型號 UH-60J和UH-60JA
　　S-70B
　　美國海軍型號 SH-60B、MH-60R、SH-60F、HH-60H
　　美國海岸警衛隊型號 HH-60J
　　日本海上自衛隊型號 SH-60J、SH-60K
　　西班牙海軍型號 HS.23
　　中國台灣海軍型號 S-70C(M)-1、S-70C(M)-2

作者: 克里斯Chris 時間: 07-4-27 18:29
美軍按照用途不同又將黑鷹分成C、E、H、M、S、U、V七大類，這僅僅是黑鷹國內型號，出口到世界其他國家的黑鷹又各有不同的型號。在其國內型號中，UH-60系列是最早服役也是用途最廣的一類，U即通用，這類黑鷹有UH-60A、 UH-60C、UH-60G、UH-60L、UH-60M、UH-60P、UH-60Q、UH-60X八種；CH-60是貨運型黑鷹，專門執行貨運任務，其中C代表貨物，該型總共出現過CH-60S一種；EH-60是特殊電子戰黑鷹，E即電子戰，共有EH-60A、EH-60B、EH-60C、EH- 60L四種；HH-60是搜索和救援型黑鷹，共有HH-60A、HH-60D、HH-60E、HH-60G、HH-60H、HH-60J六種；MH-60 是多用途黑鷹，主要用於執行特戰，共有MH-60A、MH-60G、MH-60K、MH-60L、MH-60S五種；SH-60是反潛型黑鷹，共有SH- 60B、SH-60F、SH-60R三種；VH-60是政要人員專用運輸機，共有VH-60A、VH-60N三種型號。

作者: 克里斯Chris 時間: 07-4-27 18:31
補充：黑鷹計畫

（知識）

1993年10月3日，一個匯集了美國三角洲特種部隊和突擊隊員由123人組成的精銳部隊進入索馬利亞首都摩加迪休( Mogadishu)，他們的任務是抓捕謀殺了24名聯合國維和人員的索馬利亞大軍閥艾迪德(Mohammed Farah Aidid)，結果遭到了索馬利亞遊擊部隊的猛烈抵抗，兩架UH-60黑鷹直升機被擊落，原定1小時的任務拖延了15個小時，而且造成美國士兵戰死18人，受傷73人。索馬利亞方面估計約有500至1000名民兵死亡，3000至4000個普通民眾受到波及（由於欠缺準確的情報管道，各方估計的數字落差非常大）。

作者: 克里斯Chris 時間: 07-4-27 18:31
美國出兵索馬利亞始末：

1991年索馬利亞發生暴動，首都摩加迪休陷入無政府狀態，接著索國南部又爆發了內戰，農民都逃進叢林裏，饑荒嚴重。暴動者出現內訌，美駐索馬利亞大使館和中情局駐摩加迪休站的工作人員乘直升機撤離，聯合國停止了饑荒救助行動。1992年底，布希總統派2.5萬名美國軍人開赴索馬利亞，目的是保證聯合國救援物資的發放。這就是所謂的“恢復希望”行動。1993年5月，由於救援工作進展順利，美國撤出了大部分軍隊，把索馬利亞交給了聯合國維和部隊。聯合國任命退役的美國海軍上將喬納桑·霍維為聯合國駐索馬利亞的高級代表。這個時候，法拉赫·艾迪德的索馬利亞民族聯盟已經成為摩加迪沙最有實力的力量。6月初，24名巴基斯坦維和人員在檢查艾迪德的電臺後被殺害。不久，霍維發佈逮捕艾迪德的命令，並懸賞2.5萬美元。7月中旬，美國陸軍向艾迪德的指揮中心實施導彈襲擊後，索馬利亞民族聯盟向美國宣戰。

美國陸軍在10月3日發動「代碼艾琳行動」（Operation Code Irene），出動精銳的遊騎兵部隊與三角洲特種部隊，配合UH-60「黑鷹」式直升機及多種戰情支援裝備，突襲摩加迪休市中心的民兵據點意圖逮捕艾迪德。在這次的行動中，美軍成功地逮捕到艾迪德的許多高階幕僚但卻任由主要目標漏網，而在任務過程中因為對叛軍勢力的低估，兩架美軍直昇機在混亂中遭到火箭推進式榴彈（RPG）擊落，並進一步導致百餘名馳援與執行任務的地面部隊深陷敵陣中無法脫離的狀況。世界各國媒體稱這場激戰「摩加迪休戰役」。

作者: 克里斯Chris 時間: 07-4-27 18:31
摩加迪休戰役是越戰結束數十年後，第一次發生的近距離肉搏戰，美國作家Mark Bowden事後收錄了自己幾篇關於此事件的專題連載，在1999年3月出版了《黑鷹計劃：一個現代戰爭的故事》（Black Hawk Down: A Story of Modern War）一書，這本書之後又由英國導演雷利史考特（Sir Ridley Scott）改拍成紀錄性電影《黑鷹計劃》（Black Hawk Down），而使衝突事件與摩加迪休這城市廣為人知。

由於摩加迪休戰役中的嚴重損失，美國決定在1994年3月31日以前，全面自索馬利亞撤軍。這件事是當時的美國柯林頓總統任內最嚴重的軍事與外交挫敗，也使得美國對第三世界國家的衝突事務之參與態度，由積極轉為保守。

作者: 克里斯Chris 時間: 07-4-27 18:34
UH-60 ブラックホーク
出典: フリー百科事典『ウィキペディア（Wikipedia）』

UH-60 ブラックホーク (UH-60 Black Hawk) は、シコルスキー社製の中程度積載能力を持つ多目的または強襲用ヘリコプターであり、20ヶ国以上で使用されている。民間型として武装を省略したS-70も販売されている。

用途：汎用ヘリコプター
製造者：シコルスキー社
運用者：主にアメリカ陸軍
初飛行：1974年10月

作者: 克里斯Chris 時間: 07-4-27 18:34
開発経緯
UH-60 ブラックホークは1972年にアメリカ陸軍が提示したUTTAS（汎用戦術輸送機システム）構想により、傑作であるUH-1 イロコイの後継機として開発された。基本設計においては、戦略輸送機C-5 ギャラクシーに搭載が可能であるよう、10tトラックと同じ容積、重量であることが求められている。またキャビン容積としては完全武装の歩兵1個分隊約10名が搭乗可能なスペースを要求されていた。3つのプロトタイプが試作され、初飛行は1974年10月に行われ、競争相手だったボーイング・バートル社の設計よりも評価された。ブラックホークの製造が決定し、1979年にUH-60Bがアメリカ軍で使用され始めた。

機体
ブラックホークは航空騎兵隊（空挺部隊）、電子戦、MEDEVAC(医療救急)などの幅広い任務で活動することができる。エアフォースワンならぬマリーンワンとしてアメリカ大統領を運ぶことさえある。空からの強襲作戦では1分隊11名とその装備か、105-mm榴弾砲（M102）と砲弾30発と6人の操作要員を、同時に運搬することもできる。2,600ポンド（1,170キログラム）の積荷、ヘリで吊り下げる形であれば9,000ポンド（4,050キログラム）の積荷を運ぶこともできる。またESSSを裝着することにより追加される左右2箇所ずつのハードポイントにAGM-114ヘルファイア対戦車ミサイル4連装ランチャー、2.75インチ(約70mm)19連装ロケット弾ポッド、ガンポッド、増槽などを搭載することもできる。このためAH-64 アパッチの開発費が高騰した際にはこれを代わりに利用することも検討された。またブラックホークはGPSなどの最新の航空電子機器を装備している。

実戦
実戦には湾岸戦争、モガディシュの戦闘、アフガニスタン戦争、イラク戦争など、近年のアメリカが関与した戦争・戦闘にはほとんど参加しているが、運用方法から極低空を低速で飛行することが多く、個人携行対空ミサイルや小火器からの対空砲火などの餌食になりやすい。そのため、これらの戦闘によって数多くの機体と兵士を失った。なお、モガディシュの戦闘において、アイディード将軍派の民兵の攻撃によって2機が撃墜された際の顛末は、映画『ブラックホーク・ダウン』において詳細に描かれている

作者: 克里斯Chris 時間: 07-4-27 18:35
派生型
汎用ヘリコプターであるS-70は、数多くの派生型も生産されている。それぞれのバージョンによって製造費用も異なり、例えばUH-60L ブラックホークは590万ドルだが、空軍のMH-60G ペイヴホークは1020万ドルの費用がかかる。民間向けにはS-70の名称で販売されている。

SH-60 シーホーク
アメリカ海軍では、1983年に水上戦闘艦搭載用のSH-60B シーホークを、1988年に空母艦載用のSH-60Fを受け取った。SH-60はUH-60の対潜哨戒機バージョンであり、レーダーなどの哨戒機器と対潜兵器を搭載できる。詳細は項目を参照。

HH-60 / MH-60
HH-60シリーズは、遭難した航空隊員や戦争中に孤立した人間を救助することを主な目的として、UH-60を改造したものである。

空軍は当初、UH-60の燃料搭載量を増やしたHH-60D ナイトホークを運用していたが、1982年にはこれを大幅に改良したHH-60G ペイヴホークを採用した。600ポンド（270キログラム）の運搬能力がある250フィート（75メートル）のケーブルをもった救助用の巻き上げ機や、脱着可能な空中給油装置が装備されている。武装はサイドワインダーもしくはスティンガーといった空対空ミサイルの搭載も可能となっている。

同系の機体として、陸軍が特殊部隊の強襲作戦に用いるMH-60シリーズも存在する。こちらはMH-60G ペイヴホークの他、高価な電子装備を搭載したMH-60K ブラックホークや、UH-60Lの設計を反映させたMH-60L ブラックホークが存在する。特にMH-60Lはモガディシュの戦闘に投入されたことで知られる。

HH-60H レスキューホーク / HH-60J ジェイホーク

HH-60J Jayhawkアメリカ海軍では、遭難した艦載機パイロットなどを救助したり、Navy SEALsの作戦を支援したりするため、HH-60H レスキューホークと呼ばれる機体を運用している。また、沿岸警備隊でも救難や密輸取締りなどを目的として1992年にHH-60J ジェイホークを導入した。これらは空軍向けのHH-60と同じような装備を持つ一方、艦上運用を前提としているため、胴体構造はSH-60シリーズをベースとしている。

なおアメリカ海軍ではHH-60Hの後継としてMH-60Sへの切り替えを進めているが、こちらはむしろ陸軍向けのUH-60Lに似た機体となっている。

VH-60N プレジデントホーク
アメリカ海兵隊が運用する政府専用ヘリコプターとして、VH-60N プレジデントホークが存在する。ホワイトハウスでよく見られるVH-3Dや、その後継機であるVH-71に比べ、輸送機への搭載が比較的容易であることを利用して外遊に用いられる。その分キャビンが非常に狭く、要人用としては乗り心地が劣るとして不評である。

作者: 克里斯Chris 時間: 07-4-27 18:35
採用国
S-70シリーズは、アメリカ軍での使用が最も有名だが、他にも日本の自衛隊、アルゼンチン、オーストラリア、バーレーン、ブルネイ、中国、コロンビア、エジプト、イスラエル、マレーシア、メキシコ、モロッコ、フィリピン、サウジアラビア、韓国、台湾、トルコの軍隊でも使われている。

日本
現在、アメリカ本国以外では最大のカスタマーである日本の自衛隊では、日本独自の改良を施した機体を三菱重工業がライセンス生産して運用している。日本の自衛隊向けの機種は末尾に"J"が付与されるものが多いが、HH-60J ジェイホークは全く無関係である。

航空自衛隊
UH-60J 救難ヘリコプター：1990年（平成2）配備開始、31機導入（平成18年現在も調達中）、40機取得予定。

V-107の後継として、アメリカ陸軍のUH-60Aをベースに改良し、赤外線暗視装置、航法気象レーダー、機体側面にバブルウインドウを装備している。全備重量9,900kg。U-125Aと組んで運用。長らく救難用に白と黄色の塗装であったが、2005年（平成17）生産分からダークブルーの洋上迷彩塗装に更新中である。チャフ/フレア・ディスペンサーを装備してある機体もある。空中受油機能を追加すると共に自衛用の7.62mm機関銃の装備も検討されている。
配備基地
千歳基地：千歳救難隊
秋田分屯基地：秋田救難隊
松島基地：松島救難隊
百里基地：百里救難隊
小松基地：小松救難隊
小牧基地：小牧救難隊
芦屋基地：芦屋救難隊
新田原基地：新田原救難隊
那覇基地：那覇救難隊

作者: 克里斯Chris 時間: 07-4-27 18:35
海上自衛隊
UH-60J 救難ヘリコプター：1990年（平成2）配備開始、19機導入（平成18年現在も調達中）。

S-61の後継として導入。空自の機体とほぼ同じだが、海自独自の装備がある為に全備重量が10,000kgに増えた。増槽タンクのパイロンはHH-60用に変更されている。こちらは白とレッドオレンジの塗装である。なお、海自では哨戒機SH-60Jも103機採用し、続いてSH-60Kを50機程度導入しているが、詳細は当該項目を参照。
配備基地
八戸航空基地：第2航空群八戸救難飛行隊
下総航空基地：下総教育航空群下総教育飛行隊
厚木航空基地：第4航空群厚木救難飛行隊
硫黄島航空基地：第4航空群硫黄島救難飛行隊
小月航空基地：小月教育航空群小月救難飛行隊
徳島航空基地：徳島教育航空群徳島救難飛行隊
鹿屋航空基地：第1航空群鹿屋救難飛行隊

作者: 克里斯Chris 時間: 07-4-27 18:36
陸上自衛隊
UH-60JA 多用途ヘリコプター：1997年（平成9）配備開始、25機導入（平成18年現在も調達中）。

アメリカ陸軍のUH-60L多用途ヘリをベースに改良した。航空輸送等に使用されることから、J型の赤外線暗視装置、航法気象レーダーに加えて、赤外線排出抑制装置やワイヤー・カッター等、チャフ/フレア・ディスペンサーを追加装備、燃料容量の増加で航続距離を1,295kmに延長。第1混成団や西部方面普通科連隊を那覇駐屯地から先島諸島・尖閣諸島へ機動展開させることが可能になり、日本の防空識別圏のほぼ全てをヘリでカバーできるようになった。装備や燃料は増えたが、全備重量は9,000kgと削減されている。当初米陸軍同様、対戦車ミサイルやロケット・ランチャーの装備をする計画だったが、予算の関係で見送られた。
配備駐屯地
北宇都宮駐屯地：第12旅団第12ヘリコプター隊第1飛行隊
霞ヶ浦駐屯地：航空学校霞ヶ浦校
立川駐屯地：東部方面航空隊東部方面ヘリコプター隊
明野駐屯地：航空学校
滝ヶ原駐屯地：航空学校教育支援飛行隊
那覇駐屯地：第1混成団第101飛行隊

作者: 克里斯Chris 時間: 07-4-27 18:36
スペック (UH-60J)

UH-60A 三面図乗員：最低2名
全長：19.76 m
全高：約3.7 m
ローター直径：16.36 m
非装備時重量：10.1 トン
最大離陸重量：11,113 kg
最高速度：約357 km/時
戦闘行動半径：約680 km
最大航続距離：約2,220 km
実用上昇限度：5,790 m
上昇率：3.6 m/s
武装
固定武装：無し
ドアに12.7mm重機関銃M2を装備可能・両側面の窓にMAG7.62mm機関銃を装備可能

作者: 克里斯Chris 時間: 07-4-27 18:36
（一）黑鷹系列

1.優點

(1)防衛性能優異：黑鷹系列UH-60型直升機的戰場存活性優異，機身基本上可抵擋小口徑武器的直接射擊，機組員座椅也配備裝甲保護，可抵擋23公厘砲彈攻擊。

(2)衝擊力低：機體與起落架經過特別設計，除機體能有效減緩高速墜毀時的衝擊力，駕駛座椅、起落架也都裝有吸收撞擊能量的裝置。

(3)系統強化：機上的燃料系統具有自封裝置，飛控系統也經過強化，戰場上的維修作業十分簡易。

作者: 克里斯Chris 時間: 07-4-27 18:36
2.配備：黑鷹式配備2具通用電機公司T700-GE-700型渦輪軸發動機，每具出力1,622軸馬力，搭配以鈦金屬與玻璃纖維複合材料製造的四葉式主旋翼，具備良好的貼地飛行能力（NOE）。機內油箱總容量1,360公升，另可在機艙內加裝共1,400公升的2具油箱，或1,740公升外掛副油箱。

3.編制：基本編制包括2名飛行員及1名機工長，機艙內配備通風及加溫設備，最多可搭載11名全副武裝士兵的1個完整步兵班。若要執行醫療任務，則能在拆除8個座椅後，載運4具擔架及1名醫官。

4.自衛武器：機身側邊可加裝兩挺7.62公厘或12.7公厘機鎗，此外利用M144型武裝次系統，則可在艙門邊架裝M60D型7.62公厘機鎗各一挺。機上其他裝備還有VHF、UHF無線電機、敵我識別裝置，以及保密語音通訊系統、衛星通訊設備，並能加裝M130型通用撒布器，以發射干擾絲及熱燄彈。此外，機腹裝有1具貨物掛鉤，最重可吊掛4,072公斤裝備，因此能夠吊掛、搭載1門105公厘榴砲、6名砲兵及30發砲彈，直接進行砲陣地轉換作業。

作者: 克里斯Chris 時間: 07-4-27 18:36
5.機型

(1)UH-60A型：於1974年10月第一次試飛，巡航速率每小時257.43公里，續航力2.3小時，最大航程592.64公里，機艙內可載重1197.5公斤，外掛重量為3628.8公斤。UH-60A型直升機於1978～1989年間生產，因此機隊自2002年開始陸續達到25年的服役壽限，為了能繼續服役至2030年，美國陸軍目前已展開延壽計畫（SLEP）。

(2)UH-60L型：1989年10月，UH-60A型直升機在改良機上的傳動系統後，成為UH-60L型。UH-60L型換裝了T700-GE-701C型發動機，動力較UH-60A型增加24％，發動機每具出力1,890軸馬力，同時在高空、高溫環境的性能也較佳。此外，更換新型齒輪箱，並採用S-70B型的飛控系統，最大巡航速率每小時294.47公里，續航力2.1小時，最大航程566.71公里。

UH-60L型的外掛重量為4082.4公斤，並可加裝外掛支援系統（ESSS），包括4具可拆式掛架，在攜掛副油箱後可延長航程到2129.8公里，並可攜掛飛彈、火箭莢艙、機砲及電戰莢艙、布雷裝置等，最多將可掛載16枚地獄火雷射導引反裝甲飛彈，並在機艙內裝載額外的16枚地獄火飛彈。至1997年止，美國陸軍總共採購了483架UH-60L型，並於2002年10月，簽訂為期5年的合約，增購80架。

作者: 克里斯Chris 時間: 07-4-27 18:37
(3)UH-60M 未來黑鷹標準型：2004年4月，美國陸軍開始進行黑鷹式改良計畫，預計超過1,500架的UH-60系列直升機，全部性能將提升至 UH-60M型的標準。第一架UH-60M原型機於2003年9月首次試飛成功，預計自2006年起服役，並使該型直升機的服役壽限延長至2025年。

UH-60M型的改良項目，除了以1553 匯流排為基礎的玻璃式座艙設計與航電裝置，其中包括4具多功能顯示器、先進飛控電腦之外，還換裝寬翼弦複合材料翼樑主旋翼，並強化機身結構，配備先進紅外線抑制裝置，並將換裝新研發的通用電機公司T700-GE-701D型發動機。

(4)UH-60Q 醫療後送機：UH-60Q型是由UH-60A型改良而成的醫療後送直升機，有效提升美軍在傷患後送途中的醫療救護能力。UH-60Q型採用與 UH-60L型直升機相同的發動機，編制機組員3名，最多可搭載6具擔架，機艙內裝有機上氧氣產生裝置、改良式環境控制系統、病人監測裝置等，並配備外掛電動吊救絞盤。

作者: 克里斯Chris 時間: 07-4-27 18:37
(5)MH-60G、K 特戰專用機

            A.MH-60G型鋪鷹式（Pave Hawk）特戰直升機：採用2具T700-GE-701C型發動機，輸出動力1,630軸馬力，飛行速率每小時294.4公里，最大起飛重量9,900公斤。機上裝有自動飛行控制系統，主旋翼配備除冰裝置，主旋翼與機尾均可摺收。此外還配備全天候雷達、伸縮式空中加油管與機艙內輔助油箱，吊救絞盤可負重270公斤，機腹另有1具荷重3,600公斤的貨物掛鉤。

               MH-60G型直升機的機組員包括2名飛行員及機工長、射手各1名，可配備兩挺7.62公厘迷你機鎗，自1982年起服役，美國空軍特戰指揮部共編配10架。作戰任務包括在日、夜間或不良氣候下為特戰部隊實施潛入、撤出與再補給作業，此外也可擔負戰鬥搜救任務。

         B.MH-60K型：是用於執行長程低空穿透任務的特戰直升機，可在漆黑夜晚、不良天候與敵人領土內作業，配備2具T700-GE-701C型發動機，每具輸出1,843軸馬力。MH-60K 型裝有先進的整合航電裝備、多功能顯示器、數位地圖產生器、前視紅外線偵測儀，以及多模式地形追沿雷達等。除了空中加油管，也能加裝2具外掛油箱。在自衛能力方面，可加裝兩挺12.7公厘機槍或兩挺M134型7.62公厘迷你機鎗，另外還搭配雷達警告系統、紅外線反制裝置。

作者: 克里斯Chris 時間: 07-4-27 18:37
(6)HH-60G 長程搜救機：同屬鋪鷹式的HH-60G型長程搜救直升機，主要用於執行戰鬥搜救任務，以及特戰部隊的部署、再補給，目前編配美國空軍、後備空軍與航空國民兵。機上除配備空中加油管，駕駛艙中還裝有油料管理面板，飛行員也可配戴夜視鏡，其他裝備還包括慣性導航系統、彩色氣象／地圖測繪雷達、衛星通訊裝置與前視紅外線儀等。

            HH-60G型的機組員包括2名飛行員、1名機工長與2名搜救人員（PJ），機艙內可載運8～10人。吊救絞盤可吊掛1具擔架，或以叢林穿刺器一次吊起3個人。機上除了APR-39A（V）1型雷達警告接收器、ALQ-144A型紅外線反制裝置與M130型撒布器外，側窗還可架設 M60、M240或GAU-2B型機鎗，艙門邊也可各裝置一挺12.7公厘機鎗。

         (7)HH-60H型搜救直升機：配備機腹掛鉤，編制4名機組員，另可搭載8名人員，能執行垂直運補（VERTREP）、後勤、打擊救援、特戰支援、醫療後送、搜救與反地面打擊等任務。

         (8)HH-60J 型：美國海岸防衛隊使用的HH-60J型Jay-hawk式直升機，主要執行搜救、近岸執法、掃毒與環保等勤務。

         (9)EH-60A、B 電子反制機

         A.EH-60A型：是美國陸軍執行電子反制任務的機型，機身外加裝特殊的天線，以攔截、反制敵人的通訊，發動機與UH-60A型相同。

         B.EH-60B型：執行距外目標搜獲任務，可偵測戰場上敵軍的動態，再將資訊傳輸到地面接收站。

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