Gyundoan-Han GH-36 Mulsuri: Difference between revisions
(Created page with "{{WIP}} The '''Gyundoan-Han GH-36 "Mulsuri"''' (Osprey) is a twin-turbine-engine heavy {{wp|Gyrodyne|compound}} {{wp|utility helicopter}} designed in Menghe by the Gyundoan-H...") |
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===GH-36D=== | ===GH-36D=== | ||
The GH-36D was specially developed in 2017 to test the feasibility of carrying out heliborne air assaults across the Strait of Portcullia. It has a refueling probe like the GH-36N, but retains the hull sponsons and rear cargo door of the GH-36G. It also adds a winch on either side of the airframe above the forward doors, allowing transported troops to {{wp|fast-roping|fast-rope}} to the ground. The GH-36D lacks the range to make a round trip across the strait on its own internal fuel, but could top off its tanks en route and during the return. Such an operation would be extremely risky, however, and some reports suggest that Menghe's GH-36Ds will be assigned to the new class of {{wp|landing helicopter dock}} ships upon their completion. | The GH-36D was specially developed in 2017 to test the feasibility of carrying out heliborne air assaults across the Strait of Portcullia. It has a refueling probe like the GH-36N, but retains the hull sponsons and rear cargo door of the GH-36G. It also adds a winch on either side of the airframe above the forward doors, allowing transported troops to {{wp|fast-roping|fast-rope}} to the ground. The GH-36D lacks the range to make a round trip across the strait on its own internal fuel, but could top off its tanks en route and during the return. Such an operation would be extremely risky, however, and some reports suggest that Menghe's GH-36Ds will be assigned to the new class of {{wp|landing helicopter dock}} ships upon their completion. | ||
==Ship classes using the GH-36== | |||
* [[Hasŏ-class cruiser]] | |||
* [[Insŏng-class destroyer]] | |||
==Users== | |||
* {{flag|Menghe}} | |||
==Specifications (GH-36N)== | ==Specifications (GH-36N)== | ||
{{Aircraft specs | |||
|ref=<!-- reference --> | |||
|prime units?=met | |||
|genhide= | |||
|crew=4 (pilot, copilot, 2 sonar operators) | |||
|capacity= | |||
|length m=16.93 | |||
|length ft= | |||
|length in= | |||
|length note=fuselage only, probe retracted | |||
|span m=4.93 | |||
|span ft= | |||
|span in= | |||
|span note= | |||
|upper span m= | |||
|upper span ft= | |||
|upper span in= | |||
|upper span note= | |||
|mid span m= | |||
|mid span ft= | |||
|mid span in= | |||
|mid span note= | |||
|lower span m= | |||
|lower span ft= | |||
|lower span in= | |||
|lower span note= | |||
|swept m=<!-- swing-wings --> | |||
|swept ft=<!-- swing-wings --> | |||
|swept in=<!-- swing-wings --> | |||
|swept note= | |||
|dia m=<!-- airships etc --> | |||
|dia ft=<!-- airships etc --> | |||
|dia in=<!-- airships etc --> | |||
|dia note= | |||
|width m=<!-- if applicable --> | |||
|width ft=<!-- if applicable --> | |||
|width in=<!-- if applicable --> | |||
|width note= | |||
|height m=5.16 | |||
|height ft= | |||
|height in= | |||
|height note= | |||
|wing area sqm= | |||
|wing area sqft= | |||
|wing area note= | |||
|swept area sqm=<!-- swing-wings --> | |||
|swept area sqft=<!-- swing-wings --> | |||
|swept area note= | |||
|volume m3=<!-- lighter-than-air --> | |||
|volume ft3=<!-- lighter-than-air --> | |||
|volume note= | |||
|aspect ratio=<!-- sailplanes --> | |||
|airfoil= | |||
|empty weight kg=9,702 | |||
|empty weight lb= | |||
|empty weight note= | |||
|gross weight kg= | |||
|gross weight lb= | |||
|gross weight note= | |||
|max takeoff weight kg=16,500 | |||
|max takeoff weight lb= | |||
|max takeoff weight note= | |||
|fuel capacity= | |||
|lift kg=<!-- lighter-than-air --> | |||
|lift lb=<!-- lighter-than-air --> | |||
|lift note= | |||
|more general= | |||
<!-- | |||
Powerplant | |||
--> | |||
|eng1 number=2 | |||
|eng1 name=Taesan T508-1 | |||
|eng1 type=Turboshaft | |||
|eng1 kw= | |||
|eng1 hp=3,200 | |||
|eng1 shp=<!-- prop engines --> | |||
|eng1 kn=<!-- jet/rocket engines --> | |||
|eng1 lbf=<!-- jet/rocket engines --> | |||
|eng1 note= | |||
|power original= | |||
|thrust original= | |||
|eng1 kn-ab=<!-- afterburners --> | |||
|eng1 lbf-ab=<!-- afterburners --> | |||
|eng2 number= | |||
|eng2 name= | |||
|eng2 type= | |||
|eng2 kw=<!-- prop engines --> | |||
|eng2 hp=<!-- prop engines --> | |||
|eng2 shp=<!-- prop engines --> | |||
|eng2 kn=<!-- jet/rocket engines --> | |||
|eng2 lbf=<!-- jet/rocket engines --> | |||
|eng2 note= | |||
|eng2 kn-ab=<!-- afterburners --> | |||
|eng2 lbf-ab=<!-- afterburners --> | |||
|eng3 number= | |||
|eng3 name= | |||
|eng3 type= | |||
|eng3 kw=<!-- prop engines --> | |||
|eng3 hp=<!-- prop engines --> | |||
|eng3 shp=<!-- prop engines --> | |||
|eng3 kn=<!-- jet/rocket engines --> | |||
|eng3 lbf=<!-- jet/rocket engines --> | |||
|eng3 note= | |||
|eng3 kn-ab=<!-- afterburners --> | |||
|eng3 lbf-ab=<!-- afterburners --> | |||
|more power= | |||
|prop blade number=1 | |||
|prop name= | |||
|prop dia m=3.39 | |||
|prop dia ft=<!-- propeller aircraft --> | |||
|prop dia in=<!-- propeller aircraft --> | |||
|prop dia note= | |||
|rot number=2 | |||
|rot dia m=14.98 | |||
|rot dia ft=<!-- helicopters --> | |||
|rot dia in=<!-- helicopters --> | |||
|rot area sqm=1,409.9 | |||
|rot area sqft=<!-- helicopters --> | |||
|rot area note= | |||
<!-- | |||
Performance | |||
--> | |||
|perfhide= | |||
|max speed kmh=450 | |||
|max speed mph= | |||
|max speed kts= | |||
|max speed note= | |||
|max speed mach=<!-- supersonic aircraft --> | |||
|cruise speed kmh=410 | |||
|cruise speed mph= | |||
|cruise speed kts= | |||
|cruise speed note= | |||
|stall speed kmh= | |||
|stall speed mph= | |||
|stall speed kts= | |||
|stall speed note= | |||
|never exceed speed kmh=460 | |||
|never exceed speed mph= | |||
|never exceed speed kts= | |||
|never exceed speed note= | |||
|minimum control speed kmh= | |||
|minimum control speed mph= | |||
|minimum control speed kts= | |||
|minimum control speed note= | |||
|range km=1200 | |||
|range miles= | |||
|range nmi= | |||
|range note= | |||
|combat range km= | |||
|combat range miles= | |||
|combat range nmi= | |||
|combat range note= | |||
|ferry range km= | |||
|ferry range miles= | |||
|ferry range nmi= | |||
|ferry range note= | |||
|endurance=<!-- if range unknown --> | |||
|ceiling m=4,850 | |||
|ceiling ft= | |||
|ceiling note= | |||
|g limits=<!-- aerobatic --> | |||
|roll rate=<!-- aerobatic --> | |||
|glide ratio=<!-- sailplanes --> | |||
|climb rate ms= | |||
|climb rate ftmin= | |||
|climb rate note= | |||
|time to altitude= | |||
|sink rate ms=<!-- sailplanes --> | |||
|sink rate ftmin=<!-- sailplanes --> | |||
|sink rate note= | |||
|lift to drag= | |||
|wing loading kg/m2= | |||
|wing loading lb/sqft= | |||
|wing loading note= | |||
|disk loading kg/m2= | |||
|disk loading lb/sqft= | |||
|disk loading note= | |||
|fuel consumption kg/km= | |||
|fuel consumption lb/mi= | |||
|power/mass= | |||
|thrust/weight= | |||
|more performance= | |||
<!-- | |||
Armament | |||
--> | |||
|guns= | |||
|bombs= | |||
|rockets= | |||
|missiles= | |||
|hardpoints= 4 | |||
|hardpoint capacity= 500 kg | |||
|hardpoint rockets= HB-8/20 rocket pod (20 × {{wp|S-8_(rocket)|H-8 rocket}}) | |||
|hardpoint missiles= [[YGG-5 Dando]], [[YDH-26]], {{wp|AGM-65_Maverick|YDH-45}} | |||
|hardpoint bombs= GYGP-500 (electro-optical) | |||
|hardpoint other= [[YŎ-35/2 torpedo]], 30mm gunpod | |||
|avionics= | |||
}} | |||
==See also== | ==See also== | ||
* [[Gyundoan-Han GH-28 Ppulsoeori]] | |||
[[Category:Menghe]] | [[Category:Menghe]] |
Revision as of 00:56, 19 January 2021
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The Gyundoan-Han GH-36 "Mulsuri" (Osprey) is a twin-turbine-engine heavy compound utility helicopter designed in Menghe by the Gyundoan-Han design bureau. It is built in a number of variants, including the utility transport GH-36G, the ASW/ASuW-focused GH-36N, and the troop transport GH-36D. Its most distinctive feature is a push rotor in the tail boom, which, in conjunction with aerodynamic stub wings and a tandem rotor, allows the helicopter to cruise at speeds of 410 kilometers per hour.
Development
The GH-36 grew out of a Navy requirement for an anti-submarine-focused helicopter which could cover a wider area of ocean than the existing Gyundoan-Han GH-28 Ppulsoeori. The designers focused on increasing the helicopter's cruise speed, which would allow it to deploy a larger sonobuoy field in the same span of time. Increased speed also conferred other advantages. Arriving more quickly at a transient sonar contact reduces the area of uncertainty around the submarine's possible location, as it cannot travel as far before the helicopter arrives. Once on site, a faster helicopter can also lay rows of sonobuoys more quickly, increasing the chance of detecting a submarine in a V-type search pattern.
To better exploit this increased speed, the helicopter would require more sonobuoys; to better exploit a larger sonobuoy payload, it would require greater endurance; and to better exploit greater endurance, it would require a heavier weapon load. All of these requirements resulted in increasingly large sizes for the competition entries. Because the Navy planned to use the new type on the Hasŏ-class cruisers, still in development, this was deemed to be an acceptable constraint.
Variants
GH-36G
The GH-36G is the baseline utility model which grew out of Gyundoan-Han's concept-demonstration prototype. It has no armament or hardpoints, and no sensors apart from basic navigation equipment. Crew and passengers can enter through vertically-opening clamshell doors on the right side of the cockpit, and there is a cargo ramp under the tail boom. There are also emergency exit windows to the left of the cockpit and on both sides of the fuselage aft. On the military version of the GH-36G, the cargo bay is left empty, and can be either loaded with light vehicles and supplies, or fitted with stretchers or canvas seats. This variant is mainly used for supply transport and personnel transport missions within friendly lines, including vertical replenishment of certain ship classes. The GH-36D specializes in air assault against hostile areas.
GH-36N
The GH-36N is a specially designed variant for naval operations, and the original objective of the project. It was first introduced on the Hasŏ-class cruisers and Insŏng-class destroyers. It can carry a total of 42 sonobuoys, with 30 in a reserve storage rack and 12 in two revolver assemblies ready for ejection. These are typically a mix of active and passive sonobuoys, as well as a few special-purpose sonobuoys for measuring water temperature and currents and communicating with submarines. Within the four-man crew, the assistant sonar operator is tasked with manually loading sonobuoys from the reserve rack to the ready revolvers; once back at his seat, he remotely controls the revolvers, selecting the desired sonobuoy type and ejecting it through a small hatch in the bottom of the fuselage. Because of this ejection system, the cabin is not pressurized, which limits the GH-36N's maximum safe altitude.
Unlike the GH-36G and GH-36D, which have large sponsons on either side of the fuselage, the GH-36N has two stub wings, each supporting two hardpoints. It is able to carry torpedoes, anti-ship missiles, and air-to-air missiles, as well as rocket pods and bombs. These diverse payload options allow the GH-36N to engage in anti-surface missions, attacking isolated corvettes, auxiliary ships, and small craft. The YGG-7 air-to-air missiles also provide a small measure of self-defense capability when operating in contested airspace. Owing to the GH-36N's slow speed, low ceiling, and poor agility, it is unlikely that it would be able to engage fighter aircraft such as the Dassault Rafale on anything close to equal terms, but air-to-air armament could complicate interception, and would allow the GH-36N to pick off enemy anti-submarine helicopters.
Because the sponsons were removed to make space for these stub wings, extra fuel tanks are carried inside the cargo compartment, which is also occupied by sonobuoy storage, sonar-processing computer equipment, and the sonar operator stations. An extendable boom probe on the lower right corner of the fuselage allows for in-flight refueling from slow-flying fixed-wing aircraft, though GH-36Ns seldom exploit this capability as there are no tankers in the air wings of Menghean carrier battle groups and anti-submarine battle groups.
Sensors consist of a deployable magnetic anomaly detector over the right side sponson, a surface-search radar under the fuselage for detecting periscopes and snorkels, and an electro-optical sensor under the nose. Chaff/flare ejectors are installed on either side of the tail, and four jammers are spread around the airframe.
The main rotors can fold to allow easier hangar storage. The tail, however, does not fold, in part because of its thickness with twin stabilizers included and in part because of the heavy driveshaft to the psuher propeller.
GH-36D
The GH-36D was specially developed in 2017 to test the feasibility of carrying out heliborne air assaults across the Strait of Portcullia. It has a refueling probe like the GH-36N, but retains the hull sponsons and rear cargo door of the GH-36G. It also adds a winch on either side of the airframe above the forward doors, allowing transported troops to fast-rope to the ground. The GH-36D lacks the range to make a round trip across the strait on its own internal fuel, but could top off its tanks en route and during the return. Such an operation would be extremely risky, however, and some reports suggest that Menghe's GH-36Ds will be assigned to the new class of landing helicopter dock ships upon their completion.
Ship classes using the GH-36
Users
Specifications (GH-36N)
General characteristics
- Crew: 4 (pilot, copilot, 2 sonar operators)
- Length: 16.93 m (55 ft 7 in) fuselage only, probe retracted
- Wingspan: 4.93 m (16 ft 2 in)
- Height: 5.16 m (16 ft 11 in)
- Empty weight: 9,702 kg (21,389 lb)
- Max takeoff weight: 16,500 kg (36,376 lb)
- Powerplant: 2 × Taesan T508-1 Turboshaft, 2,400 kW (3,200 hp) each
- Main rotor diameter: 2× 14.98 m (49 ft 2 in)
- Main rotor area: 1,409.9 m2 (15,176 sq ft)
- Propellers: single blade, 3.39 m (11 ft 1 in) diameter
Performance
- Maximum speed: 450 km/h (280 mph; 243 kn)
- Cruise speed: 410 km/h (255 mph; 221 kn)
- Never exceed speed: 460 km/h (286 mph; 248 kn)
- Range: 1,200 km (746 mi; 648 nmi)
- Service ceiling: 4,850 m (15,910 ft)
Armament
- Hardpoints: 4 with a capacity of 500 kg,with provisions to carry combinations of:
- Rockets: HB-8/20 rocket pod (20 × H-8 rocket)
- Missiles: YGG-5 Dando, YDH-26, YDH-45
- Bombs: GYGP-500 (electro-optical)
- Other: YŎ-35/2 torpedo, 30mm gunpod