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MH-60G
PAVE HAWK
The MH-60G
Pave Hawk is a modern, medium-lift, special operations
helicopter for missions requiring medium-to-long-range
infiltration, exfiltration, and resupply of special
operations forces on land or sea. In addition, the SOF-unique
mission equipment allows this aircraft to be used for
recovery of injured special operations personnel. The
MH-60G is equipped with forward-looking infrared radar
to better enable the crew to follow terrain contours
and avoid obstacles at night. The Air Force has 55 Pave
Hawks in the active component and 25 in the Reserves.
MH-60G
Specifications
· Builder: Sikorsky
· Power Plant: 2 General Electric T700-GE or
T700-GE-01C engines
· Thrust: 1,560-1,630 shaft horsepower each
engine
· Length: 64.8 ft (17.1 meters)
· Height: 16.8 ft (4.4 meters)
· Rotary Diameter: 53.7 ft (14.1 meters)
· Speed: 184 mph
· Maximum Takeoff Weight: 22,000 lbs
· Range: 450 nautical miles (unlimited with
aerial refueling)
· Armament: Two 7.62mm miniguns
· Crew: Two officers (pilots); two enlisted
(flight engineer and gunner)
Mission
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. The MH-60G, a highly modified
variant of the UH-60A Black Hawk, offers increased capability
in range (endurance), navigation, communications, and
defensive systems. The MH-60G can be deployed to support
a full range of special air warfare activities to include
special operations, psychological operations, and civil
affairs.
EQUIPMENT
Navigation
Equipment
MH-60G navigation
equipment includes:
· Integrated navigation computer system consisting
of a ring-laser inertial navigation system
· Global positioning system
· Doppler navigation system
· TACAN
· KG-10 map display unit
· Weather avoidance radar
The MH-60G
also includes a navigation system interfaced forward
looking infrared (FLIR) system and a voice altitude
warning system to provide enhanced terrain clearance
operations. A Personnel Locator System (PLS) is installed
to enhance locating and identifying ground forces for
extraction.
Special/Auxiliary
Equipment
· All the MH-60Gs 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.
· Internal cargo tie down rings, a rescue hoist,
and an "H-bar" installation are standard
equipment as insertion/extraction devices for hoist,
fast rope, rappelling, stabo, and SPIE rig operations.
· The Pave Hawk can also be equipped with the
external stores support system.
· To extend their range, the 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 250-foot
cable with a 600-pound capacity.
· External loads can be carried on an 8,000-pound
capacity cargo hook. For shipboard operations and
to ease air transportability Pave Hawks are equipped
with folding rotor blades and tail stabilator.
· Communication systems include secure HF, UHF,
HAVE QUICK UHF, and FM radios as well as SATCOM
and digital data burst system.
Defensive
Equipment
· ALQ-144 infrared countermeasures (IRCM) system
· Hover infrared suppression system
· improved flare and chaff dispensing systems
Defensive
Armaments
Defensive
armaments include a forward cabin-mounted 7.62mm miniguns
firing either 2,000 or 4,000 rpm and cabin-mounted .50-cal
machine guns. With the addition of the external stores
support system (ESSS), the aircraft can carry fixed
forward-firing armaments for use as a defensive and
escort aircraft. Each ESSS wing can carry two 7 or 19-shot,
2.75-inch folding fin aerial rocket pods or dual 20mm
cannons/.50-cal machine guns.
Employment
The MH-60G
can be successfully employed in the low-to-medium threat
environment. As the level of threat increases above
this, the chance of detection will increase, decreasing
the probability of success. The probability of success
will also decrease as the total number of aircraft in
the mission increase due to an increased chance of detection
(i.e., larger multi-ship or dissimilar type formations).
The requirement to operate from a Forward Area Arming
and Refueling Point (FAARP) will also decrease the probability
of success due to the extended exposure time.
The MH-60G
will operate at low altitudes over land and water. The
aircraft will normally be employed as part of a larger
vertical-lift package, which may require dissimilar
multi-ship formations. The MH-60G will operate into
unprepared, unlighted, uncontrolled landing zones 50
meters or
larger in diameter.
Deployment
The MH-60G
can be deployed by airlift, sea-lift, or self-deployed.
The preferred deployment option is airlift using a C-5,
and is essential if rapid deployment is required. A
C-5 can transport a maximum of five MH-60Gs. The aircraft
can be broken down for shipment in less than 1 hour
and off-loaded and rebuilt at the location in less than
2 hours. The optimum deployment package is four MH-60Gs
via C-5. Due to the rapid tear down and buildup times,
it is normally faster to air transport the aircraft
rather than self-deploy when distances exceed 1,500
NM using aerial refueling, or 1,000 NM using ground
refueling. Deployments can be worldwide using a main
base or a limited/standby base with host support. Deployments
can be conducted in a deceptive or low-visibility mode.
The number of aircraft required and the time phasing
after notification are specified in other sources. Self-deployment
utilizing aerial refueling assets requirements are:
· One tanker aircraft, plus one spare, per four
MH-60Gs.
· Two tanker aircraft, plus one spare, per six
MH-60Gs or sea in marginal weather conditions using
minimum/no communications.
Planning
Considerations
The time
required to adequately plan for a mission varies with
the complexity and length of the mission (i.e., flight
time, number of other aircraft, types of aircraft involved
in the formation, threat, and location of the objective).
As a general rule of thumb, comprehensive mission planning
requires a minimum of 6 hours. Ideally, a tasking arrives
while the crews are in crew rest, and primary mission
planning is accomplished by unit mission planners. The
crews arrive approximately 3 hours prior to their mission
departure time and fine tune the planning.
Weather
Minimums
The MH-60G
is designed to operate in a variety of weather conditions.
Due to the use of night optical devices (NVGs and FLIR)
and color weather radar, the aircraft can operate in
very low- visibility conditions with low cloud ceilings.
However, the MH-60G is a visual meteorological conditions
(VMC) platform with weather avoidance capability.
Fuel
Endurance and Performance
Mission
endurance is increased through the use of an air refueling
probe for inflight aerial refueling. In addition, the
aircraft can be ground refueled using pressure or gravity
feed systems at forward area arming and refueling points
(FAARPS) or onboard ships. The MH-60G has a choice of
internal auxiliary fuel tanks for extended range operations.
The aircraft can be equipped with either the single,
117-gallon tank, offering 3.3 hours of aircraft operations,
or the dual, 185-gallon tanks, offering 4.5 hours of
unrefueled operations.
Mission
Effectiveness
Mission
effectiveness is highly dependent upon accurate, complete,
all-source, real-time intelligence. The MH-60G has weather
avoidance radar, but this equipment does not replace
the use of detailed, highly accurate, timely weather
forecasts for pre-mission planning.
Troop/Aircraft
Load Capacity
The aircraft
is capable of transporting 12 combat-equipped troops
in an alternate loading configuration without internal
auxiliary fuel tanks. With internal fuel tanks installed,
maximum troop capacity is 10, with an optimum load of
6.
Aircrew
Crew Qualification.
Aircrews maintain qualification in night vision goggle
(NVG) tactical operations, NVG aerial refueling, NVG
shipboard operations, and NVG overwater operations to
include rubber boat deployment ("low and slow"),
fast rope infiltration, and hoist or rope ladder exfiltration.
Standard Crew: 2 pilots, 2 flight engineers (or 1 flight
engineer and 1 aerial gunner).
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