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{{WIP}}
{|{{Infobox aircraft begin
|name= GHK-38 Wolverine
|image=
|caption=
}}{{Infobox aircraft type
|type= {{wp|Compound helicopter|Compound}} {{wp|attack helicopter}}
|national origin= [[Hallia]]<br>[[Menghe]]
|manufacturer= Gyundoan-Han
|designer=
|first flight= 25 June 2016
|introduced= 2024 (expected)
|retired=
|status= Under development
|primary user= [[Hallia]]<br>[[Menghe]]
|more users= <!--Limit TOTAL of THREE (3) 'more users' here. Please separate with <br/>. -->
|produced=
|number built=
|unit cost=
|developed from=
|variants with their own articles=
}}
|}


The '''Gyundoan-Han-Kansainyhteisön GHK-38 Wolverine''' is an advanced {{wp|attack helicopter}} jointly developed by [[Hallia]] and [[Menghe]]. The Gyundoan-Han Helicopter Corporation contributed the powerplant and general layout, while Kansainyhteisön Ilmailu was responsible for the airframe materials and electronics. There are some minor differences between the baseline variants developed in Hallia and Menghe, including the type of autocannon mounted under the hull and the spacing of the bomb suspension locks on the pylons, but most of these parts can be swapped out in production to streamline parts commonality.
The '''Gyundoan-Han-Kansainyhteisön GHK-38 Wolverine''' is an advanced {{wp|compound helicopter|compound}} {{wp|attack helicopter}} jointly developed by [[Hallia]] and [[Menghe]]. The Gyundoan-Han Helicopter Corporation contributed the powerplant and general layout, while Kansainyhteisön Ilmailu was responsible for the airframe materials and electronics. There are some minor differences between the baseline variants developed in Hallia and Menghe, including the type of autocannon mounted under the hull and the spacing of the bomb suspension locks on the pylons, but most of these parts can be swapped out in production to streamline parts commonality.


The GHK-38 uses a {{wp|compound helicopter}} configuration, with a six-bladed pusher propeller in the rear. Its main rotor uses a {{wp|coaxial rotor|coaxial configuration}} with rigid blades.
As of 2022, the GHK-38 is in late-phase development, with the first deliveries tentatively scheduled for 2024.


==Development==
===Fast Attack Helicopter Program===
In 2008, the Menghean [[Ministry of National Defense (Menghe)|Ministry of National Defense]] opened the Fast Attack Helicopter program. The goal of this program was to develop a new type of attack helicopter that would combine the speed and agility of the [[Saebyŏk SS-32 Jamjari|SS-32 Jamjari]] with the armor and payload of the [[Gyundoan-Han GH-26 Agŏ|GH-26 Agŏ]]. During the 2000s, the [[Menghean Army]] had used both of these helicopters in concert, with the SS-32 acting as a forward scout for the slower GH-26, but this division of labor had its drawbacks, including redundant sets of spare parts for two unrelated attack helicopter designs.
Menghe's two main design bureaus specializing in helicopters, Gyundoan-Han Helicopter Corporation and Saebyŏk Rotorcraft, both began work on competing prototypes. Gyundoan-Han, which had the most experience in original design work, was the initial favorite, but it struggled with many aspects of the design, particularly speed. By 2011, Gyundoan-Han had produced an independent design for a pushrotor-driven gunship with a coaxial rotor, but many of the components, including the engine, existed only on paper. No full-size prototypes of the Gyundoan-Han GH.347 design exist, but Gyundoan-Han did build a number of scale models for design expositions and wind tunnel testing; these show a stepped cockpit design and wider sponsons on either side of the cockpit.
Saebyŏk began with incremental improvements to its existing helicopter platform, the SS-32. A single SS-32 airframe was extensively modified during construction to feature a pusher propeller, a longer nose, and wider stub wings supporting three hardpoints each. This helicopter appeared at a Menghean military airshow in May 2014, and performed stunts for the audience while the announcer described it as a "new model of Army-Navy attack helicopter." Foreign press mistakenly assigned it the designation SS-36, and for a time the designation stuck, with the Menghean MoND issuing no corrections. In reality, Saebyŏk's SS.332 prototype was only meant as a testbed and concept demonstrator, and it never received a numeral designation from the MoND.
===Joint development===
Slow development continued until 2012, when representatives from [[Hallia]] expressed interest in merging the Fast Attack Helicopter program with their own plans for a new helicopter gunship. Under a division of labor negotiated the following year, Kansainyhteisön Ilmailu would contribute the airframe, electronics, and composite materials, while its Menghean partners would contribute the powerplant and general layout. Each country would then make their own modifications to the pylons and guidance systems to support locally made missiles.
At the outset, Kansainyhteisön Ilmailu opened joint development programs with both Saebyŏk and Gyundoan-Han, neither of which had produced a working prototype. By operating two redundant programs, the MoND hoped to encourage productive competition between its major design firms, while also leaving the option of choosing the final prototype with better overall characteristics.
Over the same time period, a separate department of Gyundoan-Han was working on what would later become the [[Gyundoan-Han GH-36 Mulsuri|GH-36 Mulsuri]]. Impressed with this craft's performance, Gyundoan-Han decided to speed up the design process by adapting the GH-36's powerplant to fit on the new airframe. The entire rotor assembly is shared between the two types, and the pusher propeller was borrowed as well. The two Taesan {{wp|turboshaft}} engines were moved behind the transmission, with their drive shafts leading forward rather than rearward on the GH-36, and the transmission was modified accordingly, but otherwise the two helicopters use an essentially identical propulsion system.
===GH.405===
Gyundoan-Han-Kansainyhteisön produced a working prototype under the designation GH.405. It conducted its first flight on 25 June 2016 at Menghe's Hŭksan test site. The prototype reportedly satisfied or exceeded all performance-related expectations, and Gyundoan-Han and Kansainyhteisön Ilmailu proceeded with further design work.
The original GH.405 prototype carried a 23mm {{wp|Gryazev-Shipunov GSh-23|GSh-23L}} cannon in the centerline turret, derived from the turret on the SS-32. Hallia, however, proposed switching to a 20mm rotary cannon for ammunition commonality, and the Menghean MoND insisted on a 30mm autocannon in order to achieve greater range and armor penetration.
==Design==
===Overview===
[[Image:GHK-38_Wolverine_cutaway_2022-02-19.png|400px|thumb|right|Cutaway side view of the GHK-38. Note the powerplant, and transmission, rear passenger space, ducted exhaust air interchange, and 30mm ammunition magazine.]]
The GHK-38 uses a {{wp|compound helicopter}} configuration, with a six-bladed pusher propeller in the rear to provide forward thrust. Its main rotor uses a {{wp|coaxial rotor|coaxial configuration}} with four rigid blades per level. Both the coaxial lifting rotor and the pusher propeller are driven from the same transmission by a pair of Taesan T508-1 {{wp|turboshaft}} engines, each one generating 2,400 kW (3,200 hp) of power. There is also an {{wp|auxiliary power unit}} forward of the transmission which provides power during the startup process and while grounded, though this is normally turned off during flight.
As on other attack helicopters, the crew consists of two personnel sitting in a tandem cockpit. The pilot sits in the rear, upper position, while the gunner and weapon systems operator sits in the forward, lower position. Both crew members have a full set of controls, meaning that the gunner can take over flying the helicopter if the pilot is incapacitated and the pilot can target weapon systems directly if necessary. Both crew members also have multi-function LCD screens, allowing them to receive input from different sensors and interface with different weapons.
In the rear fuselage, just behind the engines, there is an electronics access compartment with two rudimentary seats. Typically, this compartment would be used to rescue the pilot and copilot of another downed helicopter, a feature also retained on later models of the [[Gyundoan-Han GH-26 Agŏ|GH-26 Agŏ]]. In addition to electronics boxes, this rear compartment contains a basic first aid and survival kit and self-defense weapons for the downed aircrew. If no other helicopters are available, the GHK-38 can also rescue other ground personnel, including special forces and civilian VIPs, though the small size and limited amenities of the rear compartment make the GHK-38 inefficient as a transport helicopter. Outside of rescue missions, the crew can use the rear compartment to transport spare parts and personal effects when ferrying to a new base, or to deliver and recover high-value cargo. On most missions, however, the crew leave the rear compartment empty.
An unusual detail on the GHK-38 is the location of its exhaust. While most helicopters place the exhaust directly behind the turbines, the GHK-38 places it at the end of the tail boom, facing upward. Inside the fuselage, exhaust from the turbines combines with cool air drawn in through a set of vents on the roof, and the hot and cool air mix while proceeding through a pair of wide tubes in the tail, bringing the temperature of the exhaust closer to atmospheric temperature. The exhaust vent itself is beyond the main coaxial rotor, meaning that the rotor downwash does not blow the exhaust back onto the fuselage and heat up the helicopter's skin. While heavier and more complex than a conventional turbine exhaust, this system makes it harder for heat-seeking missiles to lock onto the helicopter, and also impairs detection and targeting by land-based infrared optics.
===Sensors and electronics===
The GHK-38 will enter service with a new electronic combat system developed in Hallia. It will reportedly offer a higher degree of {{wp|sensor fusion}} than previous Menghean and Hallian helicopters, providing the crew with good situational awareness, including alerting them to the presence of enemy anti-aircraft weapons detected by other platforms.
The pilot and gunner both use a version of the [[Keikō HMD|Keikō-II helmet-mounted display]], which projects target markers, threat markers, and avionics information in front of the user's eyes and allows the user to "see" icons through the floor of the cockpit. This allows either crew member to look at a target and promptly redirect the autocannon and under-nose optical unit to face it. The Keikō-II HMD also provides both crew members with night vision, allowing all-day and all-weather operations.
On top of the rotor mast, there is a millimeter-wave radar antenna in a disc-shaped enclosure. This fixed array can scan a 120-degree arc in front of the helicopter, detecting land vehicles and passing their coordinates to the crew. When used in conjunction with a downward-facing radio altimeter, this system will reportedly give the helicopter terrain-following navigation capability, allowing low-level flights through uneven terrain in low-visibility conditions.
===Armament===
[[Image:GHK-38_payload_options_2022-02-19.png|400px|thumb|right|Diagram showing possible hardpoint options for the GHK-38, based on information released in 2021.]]
The Menghean model of the GHK-38 will carry a 30mm {{wp|Shipunov_2A42|Shipunov 2A72}} autocannon in an aerodynamically faired turret underneath the fuselage. This select-fire weapon has two ammunition feeds, one containing 700 rounds of high-explosive ammunition, and one containing 440 rounds of armor-piercing ammunition. APFSDS ammunition fired from the 2A72 can defeat 85mm of steel plate (line-of-sight thickness) at 1,000 meters, and 45mm of steel plate at 3,000 meters. Unlike the select-fire 2A42, the 2A72 only has a 300rpm setting.
The GHK-38 is fitted with six hardpoints, three under each wing. The two inboard pairs are rated for payloads of up to 700 kilograms, and the outboard pair, for payloads of up to 400 kilograms. Total payload capacity is reportedly 2,400 kilograms. All six hardpoints are wired to support rocket pods and guided missile modules, and the inner four are piped to support drop tanks. In addition to rocket pods and a wide variety of anti-tank missiles, the GHK-38 can also support a number of more unique payloads, such as the [[YGG-5 Dando]] air-to-air missile, the [[YGG-5_Dando#YDJ-5|YDJ-5]] anti-radiation missile, and 23mm and 12.7mm gunpods.
===Protection and countermeasures===
The designers of the GHK-38 placed a heavy emphasis on survivability. A composite metal "bathtub" surrounds the cockpit, protecting the pilot and copilot against 23mm fire from the front and 14.5mm fire from the sides. The canopy is made of bulletproof armor glass, and is able to withstand 14.5mm ammunition. While still vulnerable to direct hits, these armor plates can also resist kinetic subminitions from {{wp|Oerlikon_GDF#Ammunition|airbursting 35mm}} and 40mm anti-aircraft rounds, as well as shrapnel from lightweight surface-to-air missiles. Gyundoan-Han claims that the rotor blades can "withstand" hits from 23mm autocannon projectiles, but it is unclear whether this refers to deflecting rounds outright or merely maintaining integrity after being penetrated.
In addition to its outside protection, the cockpit has a heavy metal armor plate behind the gunner's seat, with a heavy bulletproof glass plate above it. Both are purported to resist 14.5mm fire, though they may be able to stop 23mm projectiles slowed by the previous layer of armor. These plates help ensure that if one crew member is incapacitated, the other will still be able to fly the helicopter to safety.
As a final protective measure, the GHK-38 has a high level of {{wp|crashworthiness}}. The crew seats are designed to sink into the cockpit floor on impact with the ground, and the armored cockpit bed itself can sink into the fuselage. In the event of engine failure, a backup tension system automatically deploys the forward landing gear to further cushion an impact with the ground; the pilot and copilot can also activate this system manually. The seats in the emergency rear compartment are simple cushioned panels bolted to the floor, and meet no crashworthiness requirements.
Gyundoan-Han chose a twin-engine layout in part because it offered greater redundancy than Saebyŏk's single-engine competitor. The two turboshaft engines are separated by metal plates and fireproofing equipment, and each one has a fire-suppression system that can be triggered automatically or activated manually from the cockpit. If either engine is damaged, especially by gunfire or proximity-fused missile warheads, the helicopter is able to fly at reduced speed on a single engine in order to return to a safe landing site.
The lack of a horizontal {{wp|tail rotor}} somewhat improves survivability: unlike a conventional helicopter, the coaxial-rotor GHK-38 will not enter a tailspin if the tail rotor or its driveshaft are damaged, though it will have to transition to conventional helicopter flight. Even if the tail is completely lost, the Wolverine can still maintain a minimal degree of control through adjusting the main rotor blades, though this is only adequate for a controlled descent to the ground.
Fuel is divided between six tanks: two in the stub wings, two in the large wing roots, one forward of the gun ammunition magazine, and one aft of the rotor hub. All of these tanks are {{wp|Self-sealing fuel tank|self-sealing}} and constructed with {{wp|ballistic foam}} to reduce the risk of fire and leakage. An active two-way pump system transfers fuel between tanks to maintain stability around the center of gravity and recover fuel from leaking tanks.
All vital electronic systems and flight controls are duplicated, providing further resilience in the case of light damage to the fuselage.
===Performance===
Main power comes from two Taesan T508-2 {{wp|turboshaft}} engines, each developing 2,400 kW (3,200 hp) of power. The T508-2 is derived from the T508-1 used on the [[Gyundoan-Han GH-36 Mulsuri]], but differs in that the driveshaft protrudes from the nose of the turbine rather than its tail end. This allows the engines to be mounted behind the transmission, providing a small degree of protection against incoming fire.
Though less aerodynamically developed than some contemporary Hallian pusher-prop designs, the GHK-38 is still considerably faster than a conventional helicopter. During a test flight on 6 September 2019, the GH.405 prototype exceeded 425 km/h in level flight, comfortably surpassing its design goal. Heavy or complex payloads, however, are expected to reduce the helicopter's cruising speed.
==Specifications (GHK-38G, Menghe)==
[[Image:GHK-38_Wolverine_3-view_color_2022-02-19.png|600px|thumb|right|Three-view color image of the GHK-38 Wolverine prototype as it appeared at the Hŭksan Test Site in 2022.]]
{{aircraft specifications
<!-- If you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]].
    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= 2 (pilot and weapon systems operator)
|length main= 17.15 m
|length alt= 56 ft 3 in
|span main= 15 m
|span alt= 48 ft
|height main= 5.61 m
|height alt= 18 ft 5 in
|area main=353 m<sup>2</sup>
|area alt=3,619 ft<sup>2</sup>
|empty weight main= 6,742 kg
|empty weight alt= 14,864 lb
|loaded weight main=
|loaded weight alt=
|max takeoff weight main= 14,470 kg
|max takeoff weight alt= 31,900 lb
|engine (prop)= 2× Taesan T08-2
|type of prop={{wp|turboshaft}}
|number of props=2
|power main= 2,300 kW
|power alt= 3,600 hp
|max speed main=
|max speed alt=
|max speed more=
|cruise speed main= 400 km/h
|cruise speed alt= 215 knots, 249 mph
|cruise speed more=
|range main=
|range alt=
|range more=
|ferry range main= 2,630 km
|ferry range alt= 1,420 nmi, 1,634 mi
|ferry range more= 4× 500 L tank, full internal fuel
|combat radius main= 815 km
|combat radius alt= 440 nmi, 506 mi
|combat radius more=; with 2,000 kg (4,400 lb) payload
|ceiling main= 6,100 m
|ceiling alt= 20,000 ft
|climb rate main= 14.6 m/s
|climb rate alt= 2,950 ft/min
|loading main=
|loading alt=
|power/mass main=
|more performance=
<!--|armament= -->
|guns= 1× chin-mounted {{wp|Shipunov 2A42|2A72}} cannon with 1,140 rounds of 30×165mm ammunition (700× HE, 440× AP)
|hardpoints= Three pylons under each wing.
**Pylons 1,6: 400kg capacity
**Pylons 2,5: 600kg capacity
**Pylons 3,4: 600kg capacity
|avionics=
}}
==See also==


[[Category:Menghe]]
[[Category:Menghe]]

Latest revision as of 00:45, 20 February 2022

GHK-38 Wolverine
Role Compound attack helicopter
National origin Hallia
Menghe
Manufacturer Gyundoan-Han
First flight 25 June 2016
Introduction 2024 (expected)
Status Under development
Primary user Hallia
Menghe

The Gyundoan-Han-Kansainyhteisön GHK-38 Wolverine is an advanced compound attack helicopter jointly developed by Hallia and Menghe. The Gyundoan-Han Helicopter Corporation contributed the powerplant and general layout, while Kansainyhteisön Ilmailu was responsible for the airframe materials and electronics. There are some minor differences between the baseline variants developed in Hallia and Menghe, including the type of autocannon mounted under the hull and the spacing of the bomb suspension locks on the pylons, but most of these parts can be swapped out in production to streamline parts commonality.

As of 2022, the GHK-38 is in late-phase development, with the first deliveries tentatively scheduled for 2024.

Development

Fast Attack Helicopter Program

In 2008, the Menghean Ministry of National Defense opened the Fast Attack Helicopter program. The goal of this program was to develop a new type of attack helicopter that would combine the speed and agility of the SS-32 Jamjari with the armor and payload of the GH-26 Agŏ. During the 2000s, the Menghean Army had used both of these helicopters in concert, with the SS-32 acting as a forward scout for the slower GH-26, but this division of labor had its drawbacks, including redundant sets of spare parts for two unrelated attack helicopter designs.

Menghe's two main design bureaus specializing in helicopters, Gyundoan-Han Helicopter Corporation and Saebyŏk Rotorcraft, both began work on competing prototypes. Gyundoan-Han, which had the most experience in original design work, was the initial favorite, but it struggled with many aspects of the design, particularly speed. By 2011, Gyundoan-Han had produced an independent design for a pushrotor-driven gunship with a coaxial rotor, but many of the components, including the engine, existed only on paper. No full-size prototypes of the Gyundoan-Han GH.347 design exist, but Gyundoan-Han did build a number of scale models for design expositions and wind tunnel testing; these show a stepped cockpit design and wider sponsons on either side of the cockpit.

Saebyŏk began with incremental improvements to its existing helicopter platform, the SS-32. A single SS-32 airframe was extensively modified during construction to feature a pusher propeller, a longer nose, and wider stub wings supporting three hardpoints each. This helicopter appeared at a Menghean military airshow in May 2014, and performed stunts for the audience while the announcer described it as a "new model of Army-Navy attack helicopter." Foreign press mistakenly assigned it the designation SS-36, and for a time the designation stuck, with the Menghean MoND issuing no corrections. In reality, Saebyŏk's SS.332 prototype was only meant as a testbed and concept demonstrator, and it never received a numeral designation from the MoND.

Joint development

Slow development continued until 2012, when representatives from Hallia expressed interest in merging the Fast Attack Helicopter program with their own plans for a new helicopter gunship. Under a division of labor negotiated the following year, Kansainyhteisön Ilmailu would contribute the airframe, electronics, and composite materials, while its Menghean partners would contribute the powerplant and general layout. Each country would then make their own modifications to the pylons and guidance systems to support locally made missiles.

At the outset, Kansainyhteisön Ilmailu opened joint development programs with both Saebyŏk and Gyundoan-Han, neither of which had produced a working prototype. By operating two redundant programs, the MoND hoped to encourage productive competition between its major design firms, while also leaving the option of choosing the final prototype with better overall characteristics.

Over the same time period, a separate department of Gyundoan-Han was working on what would later become the GH-36 Mulsuri. Impressed with this craft's performance, Gyundoan-Han decided to speed up the design process by adapting the GH-36's powerplant to fit on the new airframe. The entire rotor assembly is shared between the two types, and the pusher propeller was borrowed as well. The two Taesan turboshaft engines were moved behind the transmission, with their drive shafts leading forward rather than rearward on the GH-36, and the transmission was modified accordingly, but otherwise the two helicopters use an essentially identical propulsion system.

GH.405

Gyundoan-Han-Kansainyhteisön produced a working prototype under the designation GH.405. It conducted its first flight on 25 June 2016 at Menghe's Hŭksan test site. The prototype reportedly satisfied or exceeded all performance-related expectations, and Gyundoan-Han and Kansainyhteisön Ilmailu proceeded with further design work.

The original GH.405 prototype carried a 23mm GSh-23L cannon in the centerline turret, derived from the turret on the SS-32. Hallia, however, proposed switching to a 20mm rotary cannon for ammunition commonality, and the Menghean MoND insisted on a 30mm autocannon in order to achieve greater range and armor penetration.

Design

Overview

Cutaway side view of the GHK-38. Note the powerplant, and transmission, rear passenger space, ducted exhaust air interchange, and 30mm ammunition magazine.

The GHK-38 uses a compound helicopter configuration, with a six-bladed pusher propeller in the rear to provide forward thrust. Its main rotor uses a coaxial configuration with four rigid blades per level. Both the coaxial lifting rotor and the pusher propeller are driven from the same transmission by a pair of Taesan T508-1 turboshaft engines, each one generating 2,400 kW (3,200 hp) of power. There is also an auxiliary power unit forward of the transmission which provides power during the startup process and while grounded, though this is normally turned off during flight.

As on other attack helicopters, the crew consists of two personnel sitting in a tandem cockpit. The pilot sits in the rear, upper position, while the gunner and weapon systems operator sits in the forward, lower position. Both crew members have a full set of controls, meaning that the gunner can take over flying the helicopter if the pilot is incapacitated and the pilot can target weapon systems directly if necessary. Both crew members also have multi-function LCD screens, allowing them to receive input from different sensors and interface with different weapons.

In the rear fuselage, just behind the engines, there is an electronics access compartment with two rudimentary seats. Typically, this compartment would be used to rescue the pilot and copilot of another downed helicopter, a feature also retained on later models of the GH-26 Agŏ. In addition to electronics boxes, this rear compartment contains a basic first aid and survival kit and self-defense weapons for the downed aircrew. If no other helicopters are available, the GHK-38 can also rescue other ground personnel, including special forces and civilian VIPs, though the small size and limited amenities of the rear compartment make the GHK-38 inefficient as a transport helicopter. Outside of rescue missions, the crew can use the rear compartment to transport spare parts and personal effects when ferrying to a new base, or to deliver and recover high-value cargo. On most missions, however, the crew leave the rear compartment empty.

An unusual detail on the GHK-38 is the location of its exhaust. While most helicopters place the exhaust directly behind the turbines, the GHK-38 places it at the end of the tail boom, facing upward. Inside the fuselage, exhaust from the turbines combines with cool air drawn in through a set of vents on the roof, and the hot and cool air mix while proceeding through a pair of wide tubes in the tail, bringing the temperature of the exhaust closer to atmospheric temperature. The exhaust vent itself is beyond the main coaxial rotor, meaning that the rotor downwash does not blow the exhaust back onto the fuselage and heat up the helicopter's skin. While heavier and more complex than a conventional turbine exhaust, this system makes it harder for heat-seeking missiles to lock onto the helicopter, and also impairs detection and targeting by land-based infrared optics.

Sensors and electronics

The GHK-38 will enter service with a new electronic combat system developed in Hallia. It will reportedly offer a higher degree of sensor fusion than previous Menghean and Hallian helicopters, providing the crew with good situational awareness, including alerting them to the presence of enemy anti-aircraft weapons detected by other platforms.

The pilot and gunner both use a version of the Keikō-II helmet-mounted display, which projects target markers, threat markers, and avionics information in front of the user's eyes and allows the user to "see" icons through the floor of the cockpit. This allows either crew member to look at a target and promptly redirect the autocannon and under-nose optical unit to face it. The Keikō-II HMD also provides both crew members with night vision, allowing all-day and all-weather operations.

On top of the rotor mast, there is a millimeter-wave radar antenna in a disc-shaped enclosure. This fixed array can scan a 120-degree arc in front of the helicopter, detecting land vehicles and passing their coordinates to the crew. When used in conjunction with a downward-facing radio altimeter, this system will reportedly give the helicopter terrain-following navigation capability, allowing low-level flights through uneven terrain in low-visibility conditions.

Armament

Diagram showing possible hardpoint options for the GHK-38, based on information released in 2021.

The Menghean model of the GHK-38 will carry a 30mm Shipunov 2A72 autocannon in an aerodynamically faired turret underneath the fuselage. This select-fire weapon has two ammunition feeds, one containing 700 rounds of high-explosive ammunition, and one containing 440 rounds of armor-piercing ammunition. APFSDS ammunition fired from the 2A72 can defeat 85mm of steel plate (line-of-sight thickness) at 1,000 meters, and 45mm of steel plate at 3,000 meters. Unlike the select-fire 2A42, the 2A72 only has a 300rpm setting.

The GHK-38 is fitted with six hardpoints, three under each wing. The two inboard pairs are rated for payloads of up to 700 kilograms, and the outboard pair, for payloads of up to 400 kilograms. Total payload capacity is reportedly 2,400 kilograms. All six hardpoints are wired to support rocket pods and guided missile modules, and the inner four are piped to support drop tanks. In addition to rocket pods and a wide variety of anti-tank missiles, the GHK-38 can also support a number of more unique payloads, such as the YGG-5 Dando air-to-air missile, the YDJ-5 anti-radiation missile, and 23mm and 12.7mm gunpods.

Protection and countermeasures

The designers of the GHK-38 placed a heavy emphasis on survivability. A composite metal "bathtub" surrounds the cockpit, protecting the pilot and copilot against 23mm fire from the front and 14.5mm fire from the sides. The canopy is made of bulletproof armor glass, and is able to withstand 14.5mm ammunition. While still vulnerable to direct hits, these armor plates can also resist kinetic subminitions from airbursting 35mm and 40mm anti-aircraft rounds, as well as shrapnel from lightweight surface-to-air missiles. Gyundoan-Han claims that the rotor blades can "withstand" hits from 23mm autocannon projectiles, but it is unclear whether this refers to deflecting rounds outright or merely maintaining integrity after being penetrated.

In addition to its outside protection, the cockpit has a heavy metal armor plate behind the gunner's seat, with a heavy bulletproof glass plate above it. Both are purported to resist 14.5mm fire, though they may be able to stop 23mm projectiles slowed by the previous layer of armor. These plates help ensure that if one crew member is incapacitated, the other will still be able to fly the helicopter to safety.

As a final protective measure, the GHK-38 has a high level of crashworthiness. The crew seats are designed to sink into the cockpit floor on impact with the ground, and the armored cockpit bed itself can sink into the fuselage. In the event of engine failure, a backup tension system automatically deploys the forward landing gear to further cushion an impact with the ground; the pilot and copilot can also activate this system manually. The seats in the emergency rear compartment are simple cushioned panels bolted to the floor, and meet no crashworthiness requirements.

Gyundoan-Han chose a twin-engine layout in part because it offered greater redundancy than Saebyŏk's single-engine competitor. The two turboshaft engines are separated by metal plates and fireproofing equipment, and each one has a fire-suppression system that can be triggered automatically or activated manually from the cockpit. If either engine is damaged, especially by gunfire or proximity-fused missile warheads, the helicopter is able to fly at reduced speed on a single engine in order to return to a safe landing site.

The lack of a horizontal tail rotor somewhat improves survivability: unlike a conventional helicopter, the coaxial-rotor GHK-38 will not enter a tailspin if the tail rotor or its driveshaft are damaged, though it will have to transition to conventional helicopter flight. Even if the tail is completely lost, the Wolverine can still maintain a minimal degree of control through adjusting the main rotor blades, though this is only adequate for a controlled descent to the ground.

Fuel is divided between six tanks: two in the stub wings, two in the large wing roots, one forward of the gun ammunition magazine, and one aft of the rotor hub. All of these tanks are self-sealing and constructed with ballistic foam to reduce the risk of fire and leakage. An active two-way pump system transfers fuel between tanks to maintain stability around the center of gravity and recover fuel from leaking tanks.

All vital electronic systems and flight controls are duplicated, providing further resilience in the case of light damage to the fuselage.

Performance

Main power comes from two Taesan T508-2 turboshaft engines, each developing 2,400 kW (3,200 hp) of power. The T508-2 is derived from the T508-1 used on the Gyundoan-Han GH-36 Mulsuri, but differs in that the driveshaft protrudes from the nose of the turbine rather than its tail end. This allows the engines to be mounted behind the transmission, providing a small degree of protection against incoming fire.

Though less aerodynamically developed than some contemporary Hallian pusher-prop designs, the GHK-38 is still considerably faster than a conventional helicopter. During a test flight on 6 September 2019, the GH.405 prototype exceeded 425 km/h in level flight, comfortably surpassing its design goal. Heavy or complex payloads, however, are expected to reduce the helicopter's cruising speed.

Specifications (GHK-38G, Menghe)

Three-view color image of the GHK-38 Wolverine prototype as it appeared at the Hŭksan Test Site in 2022.

General characteristics

  • Crew: 2 (pilot and weapon systems operator)
  • Length: 17.15 m (56 ft 3 in)
  • Rotor diameter: 15 m (48 ft)
  • Height: 5.61 m (18 ft 5 in)
  • Disc area: 353 m2 (3,619 ft2)
  • Empty weight: 6,742 kg (14,864 lb)
  • Max. takeoff weight: 14,470 kg (31,900 lb)
  • Powerplant: 2 × 2× Taesan T08-2 turboshaft, 2,300 kW (3,600 hp) each

Performance

Armament

  • Guns: 1× chin-mounted 2A72 cannon with 1,140 rounds of 30×165mm ammunition (700× HE, 440× AP)
  • Hardpoints: Three pylons under each wing.
    • Pylons 1,6: 400kg capacity
    • Pylons 2,5: 600kg capacity
    • Pylons 3,4: 600kg capacity

See also

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