Gyundoan-Han GH-28 Ppulsoeori: Difference between revisions
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*{{flag|Menghe}} | *{{flag|Menghe}} | ||
==Specifications== | ==Specifications (GH-28R1)== | ||
{{aircraft specifications | |||
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Please answer the following questions: --> | |||
|plane or copter?=copter | |||
|jet or prop?=prop | |||
<!-- Now, fill out the specs. Please include units where appropriate (main comes first, alt in parentheses). If an item doesn't apply, like capacity, leave it blank.--> | |||
|ref= | |||
|crew= 5 (pilot, copilot, and three sensor operators) | |||
|length main= 12.77 m | |||
|length alt= 41 ft 11 in | |||
|span main= | |||
|span alt= | |||
|height main= 5.45 m | |||
|height alt= 17 ft 10 in | |||
|area main=2 × 15.8 m<sup>2</sup> | |||
|area alt=170 ft<sup>2</sup> | |||
|empty weight main= 7,650 kg | |||
|empty weight alt= 16,870 lb | |||
|loaded weight main= | |||
|loaded weight alt= | |||
|max takeoff weight main= 12,000 kg | |||
|max takeoff weight alt= 26,500 lb | |||
|engine (prop)= {{wp|Klimov_TV3-117|GH Type 04}} | |||
|type of prop={{wp|turboshaft}} | |||
|number of props=2 | |||
|power main= 1,660 kW | |||
|power alt= 2,230 hp | |||
|max speed main= 260 km/h | |||
|max speed alt= 140 knots, 161 mph | |||
|max speed more= | |||
|cruise speed main= | |||
|cruise speed alt= | |||
|cruise speed more= | |||
|range main= 900 km | |||
|range alt= 485 nautical miles, 560 miles | |||
|range more= | |||
|ferry range main= | |||
|ferry range alt= | |||
|ferry range more= | |||
|combat radius main= | |||
|combat radius alt= | |||
|combat radius more= | |||
|ceiling main= 3,800 m | |||
|ceiling alt= 12,400 ft | |||
|climb rate main= | |||
|climb rate alt= | |||
|loading main= | |||
|loading alt= | |||
|power/mass main= | |||
|more performance= | |||
<!--|armament= --> | |||
|guns= | |||
|hardpoints= One pylon per side. Armament options for each hardpoint include: | |||
** 4 {{wp|Brimstone (missile)|YGJ-48}} anti-tank/anti-ship missiles | |||
** 8 [[YDCh-17]] anti-tank missiles | |||
** 4 [[YDCh-72]] anti-tank missiles | |||
** 1 GHB-8-20 J rocket pod with twenty 80mm rockets | |||
** 1 GHB-14-4 J rocket pod with four 140mm rockets | |||
** 1 P-500 series unguided bomb | |||
** 1 PR-500 series depth charge | |||
** 1 400mm homing torpedo | |||
** 1 23mm gun pod | |||
Additional over-wing mount for MANPADS missile tube. | |||
|avionics= | |||
** Surface-search radar | |||
** Dipping sonar | |||
** Trailing magnetic anomaly detector | |||
** 20 × sonobuoy in side ejector tube | |||
}} | |||
==See also== | ==See also== |
Revision as of 03:25, 27 July 2019
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The Gyundoan-Han GH-28 (Formal designation: 균도안-한 28호 직승기 / 균도안-恨 二八號 直升機, Gyundoan-Han ipal-ho Jiksŭnggi, "Gyundoan-Han No.28 Helicopter;" Short designation 균한-28 Gyuhan-ipal "GH-28"), also known by the nickname Ppulsoeori (뿔쇠오리, "crested murrelet"), is a utility helicopter family used by the Menghean Navy from the 1970s to the present day. It has been built in troop transport, anti-submarine warfare, and maritime search and rescue variants.
Design and development
In 1975, the Democratic People's Republic of Menghe purchased two Kamov Ka-27 helicopters from Letnia as competitors in a procurement search for the Menghean People's Navy. Though satisfied with most aspects of the design, MPN representatives requested that changes be made to suit their needs, resulting in substantial modifications to the body of the helicopter. While design work was underway, Gyundoan-Han negotiated a license agreement for the Ka-27's Klimov TV3-117 turbine engine and transmission, but did not negotiate a license for the Ka-27 itself. When the GH-28 was unveiled in 1978, its existence fed international debate over whether it had been illegally copied from the Ka-27 airframe, with Gyundoan-Han insisting that all aiframe parts apart from the powerplant and rotor set are of independent design and not subject to patent restrictions.
Like the Ka-27, the GH-28 uses a tandem rotor configuration, which eliminates the need for a tail rotor to counteract rotational torque. Once the helicopter has handed, service crews can fold the rotor blades back over the top of the fuselage, further reducing its storage space. A twin rotor also gives the GH-28 a relatively good power-to-weight ratio, allowing it to carry heavy sensor equipment (in its "N" variant) or a large cargo payload (in its "G" variant), and more stable handling in hover and descent, good for landing on a moving ship.
The GH-28 was originally ordered in two variants. The first, variant "G," was a dedicated troop transport and utility airframe, with a roomy passenger compartment and no dedicated ground-attack electronics apart from the pilot's holographic rocket sight. The second, variant "N," was a dedicated anti-submarine warfare platform, with a dipping sonar, sonobuoy rack, sea-search radar, and trailing magnetic anomaly detector. It also had room for two additional crew members who were tasked with monitoring the submarine-search electronics. Both helicopters retained external weapons pylons to carry rocket pods and homing torpedoes. Over the decades that followed, both received substantial upgrades and refits to make use of new weapons and electronics, and some new variants built around other roles were introduced.
Differences with Ka-27
Though the GH-28 is often described as a "clone" of the Kamov Ka-29, the two helicopters have a number of external differences due to Gyundoan and Han's modifications to the airframe. Notable external differences, useful for spotting and identification, include:
- The entire body is widened to match the cockpit, in contrast to the Ka-29, which becomes narrower near the hardpoint supports.
- The rudders and vertical stabilizers are more angular, and grow narrower from front to rear rather than rear to front.
- There is a centered, retractable front nosewheel, as opposed to the two non-retractable side nosewheels of the Ka-29.
- The rear landing gear sits under teardrop-shaped supports, and is retractable, with no link to the hardpoint supports.
- The door to the passenger compartment slides forward on rails, rather than opening in an up-down clamshell layout.
- The door to the pilot's compartment opens on a hinge rather than a rail.
- The window behind the pilot/copilot door windows is larger and slopes upward on the lower edge, somewhat resembling the windows on the Demirkan-Yŏng'an DY-11.
- On most versions, the external arms stores have one hardpoint per side rather than two, and they are about 33% shorter.
- The antennas and radomes under the tail boom are different, though they vary between models.
- The nose is slightly longer and rounder, and the cockpit slightly further forward.
Variants
- GH-28G:
- Original troop transport and general utility version.
- GH-28N:
- Original anti-submarine warfare version. Features a nose-mounted sea search radar, a dipping sonar at the base of the tail, and a trailing magnetic anomaly detector at the end of the tail. The troop compartment is taken up by an electronics and instruments room, and the total crew is increased to six. Unlike the Ka-27, it does not have an internal bay for sonobuoys; these are instead carried in a dispenser rack on one of the hardpoints.
- GH-28D:
- Dedicated search-and-rescue variant introduced in the 1980s. Generally similar to the GH-28G, it differs most visibly in the layout of the landing gear: the wheels are non-retractable, split one per side on the front, and are surrounded by inflatable floats, allowing the helicopter to land directly on the surface of the ocean. A small winch assembly over each door allows a rope or stretcher to be lowered into the water. The hardpoints are removed, but in their place the helicopter carries remote-controlled searchlights.
- GH-28R:
- Improved anti-submarine warfare version introduced in the 1990s. Features an entirely different sea-search radar in a new nose profile, as well as a new dipping sonar in the same compartment. The sliding doors of the crew compartment were removed entirely and replaced with a fixed, starboard-facing sonobuoy ejector system. A laser and electro-optical targeting system was installed on top of the cabin to magnify visual contacts and provide designation for certain weapons.
- GH-28M:
- A new "transport-gunship" variant used for landing troops ashore in Marine Infantry operations. It has wider wing struts with an extra pair of hardpoints, and a dual-spectrum camera and laser designator in the nose to target guided munitions. Defensive changes include the addition of an infrared jamming system, exhaust-cooling air mixers, and chaff and flare dispensers on the fuselage sides.
- GH-28B:
- Airborne early warning variant with a large air- and surface-search radar mounted under the fuselage. In flight, the array stored against the lower hull folds downward and rotates, identifying and tracking targets and linking the information back to friendly ships. The location of the radar required the use of the GH-28D's non-retractable outboard landing gear, with the floats removed. The GH-28B also adds the nose-mounted laser and electro-optical sight of the GH-28M, to visually identify targets, though without hardpoints it cannot attack with missiles.
- GH-28R1:
- Upgrade kit for the GH-28R introduced in 2015, to improve air-to-air survivability. Adds the exhaust mixers and IR jammer of the GH-28M. Also adds new mounting points, above the existing pylons, which allow the carriage of two MANPADS launch tubes in addition to the existing payload.
- GH-29:
- Civilian heavy-lifting version. Mainly intended for the export market. Potential applications include selective logging, radio tower installation, and the delivery of supplies to mountainous areas. Resembles a GH-28G with the hardpoints removed.
Operators
Specifications (GH-28R1)
General characteristics
- Crew: 5 (pilot, copilot, and three sensor operators)
- Length: 12.77 m (41 ft 11 in)
- Rotor diameter: ()
- Height: 5.45 m (17 ft 10 in)
- Disc area: 2 × 15.8 m2 (170 ft2)
- Empty weight: 7,650 kg (16,870 lb)
- Max. takeoff weight: 12,000 kg (26,500 lb)
- Powerplant: 2 × GH Type 04 turboshaft, 1,660 kW (2,230 hp) each
Performance
- Maximum speed: 260 km/h (140 knots, 161 mph)
- Range: 900 km (485 nautical miles, 560 miles)
- Service ceiling: 3,800 m (12,400 ft)
Armament
- Hardpoints: One pylon per side. Armament options for each hardpoint include:
Additional over-wing mount for MANPADS missile tube.
Avionics
- Surface-search radar
- Dipping sonar
- Trailing magnetic anomaly detector
- 20 × sonobuoy in side ejector tube