# CH-47 ChinookCH-47 is a tandem rotor helicopter developed by American rotorcraft company Vertol and manufactured by Boeing Vertol. The Chinook is a heavy-lift helicopter that is among the heaviest lifting Western helicopters.# Cockpit+—————–+——————————————————————————————————————————————————————————————————————-+ |First flight |1961 | +—————–+——————————————————————————————————————————————————————————————————————-+ |Length |30.14 m (98 ft, 10.7 in) | +—————–+——————————————————————————————————————————————————————————————————————-+ |Height |5.68 m (18 ft, 7.8 in) | +—————–+——————————————————————————————————————————————————————————————————————-+ |Ceiling |6,096 m (20,000 ft) | +—————–+——————————————————————————————————————————————————————————————————————-+ |Range |200 nm (370.4km) | +—————–+——————————————————————————————————————————————————————————————————————-+ |Weight |50,000 lb (22,680 kg) | +—————–+——————————————————————————————————————————————————————————————————————-+ |Power plant |One Volvo Aero RM12 afterburning turbofan | +—————–+——————————————————————————————————————————————————————————————————————-+ |Speed |302 km/h (170 KTAS) | +—————–+——————————————————————————————————————————————————————————————————————-+ |Accommodation|3 crew or 2 pilots + 2 crew chiefs/gunners | | | | | |33-55 Troops or 24 stretchers and 3 attendants | +—————–+——————————————————————————————————————————————————————————————————————-+ |Armament |Up to 3 pintle-mounted medium machine guns (1 on loading ramp and 2 at shoulder windows), generally 7.62 mm (0.300 in) M240/FN MAG machine guns, and can be armed with the 7.62 mm M134 Minigun rotary machine gun.| +—————–+——————————————————————————————————————————————————————————————————————-+
# UH-60The UH-60 is a four-blade, twin-engine, medium-lift utility military helicopter manufactured by Sikorsky Aircraft. # Cockpit+—————–+—————————————————————————————————————————————————————————————————————————-+ |First flight |1961 | +—————–+—————————————————————————————————————————————————————————————————————————-+ |Length |64 ft 10 in (19.76 m) including rotors | +—————–+—————————————————————————————————————————————————————————————————————————-+ |Height |16 ft 10 in (5.13 m) | +—————–+—————————————————————————————————————————————————————————————————————————-+ |Ceiling |19,000 ft (5,800 m) | +—————–+—————————————————————————————————————————————————————————————————————————-+ |Range |3,000 km maximum | +—————–+—————————————————————————————————————————————————————————————————————————-+ |Weight |22,000 lb (9,979 kg) | +—————–+—————————————————————————————————————————————————————————————————————————-+ |Power plant |2 × General Electric T700-GE-701C/D turboshaft engines, 1,994 shp (1,487 kW) each | +—————–+—————————————————————————————————————————————————————————————————————————-+ |Speed |159 kn (183 mph, 294 km/h) | +—————–+—————————————————————————————————————————————————————————————————————————-+ |Accommodation|2 pilots + 2 crew chiefs/gunners | +—————–+—————————————————————————————————————————————————————————————————————————-+ |Armament |Guns: | | | | | |2 × 7.62 mm (0.30 in) M240 machine guns | | | | | |2 × 7.62 mm (0.30 in) M134 minigun or | | | | | |2 × 12.7 mm (0.50 in) GAU-19 gatling guns | | | | | |Hardpoints: 4, 2 per ESSS stub wings, with provisions to carry combinations of: | | | | | |Rockets: 70 mm (2.75 in) Hydra 70 unguided rockets in either a 7 tube (M260) or 19 tube (M261) pod. | | | | | |Missiles: Up to 4x AGM-114 Hellfire laser guided air-to-ground missiles or 2x AIM-92 Stinger heat seeking air-to-air missiles per hardpoint. The Hellfire launcher rails can also be equipped with M260 (7 tube) Hydra pods.| | | | | |Other: 7.62 mm (0.30 in), 12.7 mm (0.50 in), 20 mm (0.787 in), or 30 mm (1.18 in) M230 gun pods | | | | | |Bombs: Can be equipped with VOLCANO minefield dispersal system. | +—————–+—————————————————————————————————————————————————————————————————————————-+# MH-6 LOH & AH-6 Light Observation Helicopter (LOH) that could perform personnel transport, escort and attack missions, casualty evacuation, and observation and has a single, six-bladed main rotor and four-bladed tail rotor. # Cockpit
+—————–+——————————————————————————————–+ |First flight |1988 | +—————–+——————————————————————————————–+ |Length |32 ft 7.2 in (9.936 m) including rotors | +—————–+——————————————————————————————–+ |Height |8 ft 9 in (2.67 m) | +—————–+——————————————————————————————–+ |Ceiling |18,700 ft (5,700 m) | +—————–+——————————————————————————————–+ |Range |232 nmi (267 mi, 430 km) at 5,000 ft (1,524 m) | +—————–+——————————————————————————————–+ |Weight |3,100 lb (1,406 kg) | +—————–+——————————————————————————————–+ |Power plant |1 × Allison T63-A-5A or T63-A-700 turboshaft engine, 425 hp (317 kW) for take-off (de-rated)| | | | | |375 shp (280 kW) at maximum continuous rpm | +—————–+——————————————————————————————–+ |Speed |152 kn (175 mph, 282 km/h) | +—————–+——————————————————————————————–+ |Accommodation|2 crew and up to 6 passengers | +—————–+——————————————————————————————–+ |Armament |Guns: | | | | | |2× 12.7×99mm (.50 BMG) GAU-19; or | | | | | |2× 7.62×51mm NATO M134 Minigun | | | | | |Rockets: | | | | | |2× LAU-68D/A 7-tubes rocket pods firing 2.75 in (70 mm) Hydra 70 rocket projectiles | | | | | |Missiles: | | | | | |4× AGM-114 Hellfire or | | | | | |4× FIM-92 Stinger | +—————–+——————————————————————————————–+# Mi-8 The Mil Mi-8 (Russian: Ми-8, NATO reporting name: Hip) is a medium twin-turbine helicopter, originally designed by the Soviet Union in the 1960s and introduced into the Soviet Air Force in 1968.# Cockpit | First flight | 1961 | | —————– | —————————————————————————————————————————————————————— | | Length | 18.4 m (60 ft 4 in) | | Height | 5.5 m (18 ft 1 in) | | Ceiling | 5,000 m (16,000 ft) | | Range | 3,000 km maximum | | Weight | 13,000 kg (28,660 lb) | | Power plant | 2 × Klimov TV3-117MT turboshaft engines, 1,454 kW (1,950 hp) each | | Speed | 2,200 km/h | | Accommodation | 3 crew and/ or 24 passengers or 12 stretchers and seat for 1 medical attendant or 4,000 kg (8,800 lb) on internal/external hardpoints | | Armament | 4,000 kg (8,818 lb) of disposable stores on six hardpoints, including 57 mm S-5 rockets, bombs, or 9M17 Phalanga ATGMs and one or two side-mounted PK machine guns |# Harbin Z-20Z-20 is a Chinese medium-lift utility helicopter produced by the Harbin Aircraft Industry Group (HAIG). It was first flown on 23 December 2013 and has a maximum takeoff weight in the range of 10 tons (22,000 lb). The Z-20 can operate from locations above 4,000 m (13,000 ft) in altitude as well as from the Liaoning aircraft carrier# Cockpit| First flight | 2013 | | —————– | —————————————————————————————————————————— | | Length | 65 ft 7 in (20 m) (approx.) | | Height | 17 ft 5 in (5.3 m) (approx.) | | Ceiling | 50,000 feet | | Range | 3,000 km maximum | | Weight | 14,000 kg | | Power plant | 2 × WZ-10 turboshaft engines, 2,682 shp (2,000 kW) each (maximum) | | Speed | 2,200 km/h | | Accommodation | 2 crew and/ or 2,200 lb (1,000 kg) of cargo internally, including 12–15 troops, and ~8,800 lb (4,000 kg) of cargo externally | | Armament | Guns: provision for machine guns |# Changhe Z-8GZ-8G is a medium-lift transport helicopter developed by Changhe Aircraft Industries Corporation (CAIC) to replace the Changhe/Harbin Z-8.# Cockpit+—————–+————————————————————–+ |First flight |2014 | +—————–+————————————————————–+ |Length |23.05 m (75 ft 7 in) (overall, rotors turning) | +—————–+————————————————————–+ |Height |7 m (23 ft 0 in) | +—————–+————————————————————–+ |Ceiling |9,000 m (29,528 ft) | +—————–+————————————————————–+ |Range |3,000 km maximum | +—————–+————————————————————–+ |Weight |13,800 kg (30,360 lb) | +—————–+————————————————————–+ |Power plant |3 × WZ-6C turboshafts | +—————–+————————————————————–+ |Speed |336 km/h (209 mph, 181 kn) | +—————–+————————————————————–+ |Accommodation|2 crew | | | | | |27-30 troops or | | | | | |15 stretchers or | | | | | |small vehicles or 5 tons of cargo to a range of up to 1000 km.| +—————–+————————————————————–+ |Armament |Up to 4 Yu-7 ASW torpedoes or YJ-9 anti-ship missiles | | | | | |Up to 32 sonobuoys | +—————–+————————————————————–+# Harbin Z-9Z-9 is a Chinese military utility helicopter with civilian variants. It is a licensed variant of the French Eurocopter AS365 Dauphin, and is manufactured by Harbin Aircraft Manufacturing Corporation.# Cockpit| First flight | 1981 | | —————– | ————————————————————————————————————————————————————- | | Length | 12.11 m (39 ft 9 in) | | Height | 4.01 m (13 ft 2 in) | | Ceiling | 4,500 m (14,800 ft) | | Range | 3,000 km maximum | | Weight | 4,100 kg (9,039 lb) | | Power plant | 2 × Zhuzhou Aeroengine Factory WZ-8A turboshaft, 632 kW (848 hp) each | | Speed | 305 km/h (190 mph, 165 kn) | | Accommodation | 1 or 2 crew and /or 10 passengers or 1,900 kg (4,189 lb) payload internal, 1,600 kg (3,527 lb) payload slung | | Armament | 2 fixed 23 mm Type 23-2 (AM-23) cannon on attack variants. Pylons for rockets, gun pods, ET52 torpedo, HJ-8 anti-tank missiles, or TY-90 air-to-air missiles. |# UH-1 VenomUH-1 a twin-engine, medium-sized utility helicopter built by Bell Helicopter under the H-1 upgrade program of the United States Marine Corps. One of the latest members of the numerous Huey family, the UH-1Y is also called “Yankee”, based on the NATO phonetic alphabet pronunciation of its variant letter. Upgrades pilot avionics to a glass cockpit, adds further safety modifications, and provides the UH-1 with a modern forward-looking infrared system. Engine power was increased. Its most noticeable upgrade over previous variants is a four-blade, all-composite rotor system designed to withstand up to 23 mm rounds. By replacing the engines and the two-bladed rotor system with four composite blades, the Y-model returns the Huey to the utility role for which it was designed.
# Cockpit| First flight | 2001 | | —————– | —————————————————————————————————————- | | Length | 58 ft 4 in (17.78 m) | | Height | 14 ft 7 in (4.45 m) | | Ceiling | 20,000 ft (6,100 m) | | Range | 130 nmi (150 mi, 240 km) with 2,182 lb (990 kg) payloa | | Weight | 18,500 lb (8,391 kg) | | Power plant | 2 × General Electric T700-GE-401C turboshaft, 1,828 shp (1,363 kW) | | Speed | 164 kn (189 mph, 304 km/h) | | Accommodation | 1 or 2 crew and/ or 6,660 lb (3,021 kg) / up to ten crashworthy passenger seats / six litters / equivalent cargo | | Armament | |# AH-1 SuperCobraAH-1 is a twin-engined attack helicopter that was developed on behalf of, and primarily operated by, the United States Marine Corps (USMC). The twin Cobra family, itself part of the larger Huey family, includes the AH-1J SeaCobra, the AH-1T Improved SeaCobra, and the AH-1W SuperCobra.# Cockpit+—————–+—————————————————————————————————————————————————–+ |First flight |1988 | +—————–+—————————————————————————————————————————————————–+ |Length |53 ft 5 in (16.28 m) with both rotors turning | +—————–+—————————————————————————————————————————————————–+ |Height |13 ft 5 in (4.09 m) | +—————–+—————————————————————————————————————————————————–+ |Ceiling |50,000 feet | +—————–+—————————————————————————————————————————————————–+ |Range |311 nmi (358 mi, 576 km) | +—————–+—————————————————————————————————————————————————–+ |Weight |10,000 lb (4,536 kg) | +—————–+—————————————————————————————————————————————————–+ |Power plant |1 × P\&W Canada T400-CP-400 (PT6T-3 Twin-Pac) turboshaft engine, 1,530 shp (1,140 kW) (de-rated from 1,800 shp (1,342 kW) for drivetrain limitations)| +—————–+—————————————————————————————————————————————————–+ |Speed |190 kn (220 mph, 350 km/h) | +—————–+—————————————————————————————————————————————————–+ |Accommodation|2 crew | +—————–+—————————————————————————————————————————————————–+ |Armament |20 mm (0.787 in) M197 3-barreled Gatling cannon in the A/A49E-7 turret (750 rounds ammo capacity) | | | | | |2.75 in (70 mm) Hydra 70 or APKWS II rockets – Mounted in LAU-68C/A (7 shot) or LAU-61D/A (19 shot) launchers | | | | | |5 in (127 mm) Zuni rockets – 8 rockets in two 4-round LAU-10D/A launchers | | | | | |TOW missiles – Up to 8 missiles mounted in two 4-round XM65 missile launchers, one on each outboard hardpoint | | | | | |AGM-114 Hellfire missiles – Up to 8 missiles mounted in two 4-round M272 missile launchers, one on each outboard hardpoint | | | | | |AIM-9 Sidewinder anti-aircraft missiles – 1 mounted on each outboard hardpoint (total of 2) | +—————–+—————————————————————————————————————————————————–+# Mi -17 The Mi-17 is an improved export version of the Mi-8 helicopter, fitted with more powerful engines and with some other minor improvements. The Mi-17 is basically an export designation.
# Cockpit+—————–+—————————————————————————————————————————————————————————————————————————————————————————————————————————————————————————————-+ |First flight |1975 | +—————–+—————————————————————————————————————————————————————————————————————————————————————————————————————————————————————————————-+ |Length |18.465 m (60 ft 7 in) | +—————–+—————————————————————————————————————————————————————————————————————————————————————————————————————————————————————————————-+ |Height |5.65 m (18 ft 6 in) | +—————–+—————————————————————————————————————————————————————————————————————————————————————————————————————————————————————————————-+ |Ceiling |6,000 m (20,000 ft | +—————–+—————————————————————————————————————————————————————————————————————————————————————————————————————————————————————————————-+ |Range |800 km (500 mi, 430 nmi) | +—————–+—————————————————————————————————————————————————————————————————————————————————————————————————————————————————————————————-+ |Weight |13,000 kg (28,660 lb) normal | | | | | |13,500 kg (29,762 lb) with under-slung load | +—————–+—————————————————————————————————————————————————————————————————————————————————————————————————————————————————————————————-+ |Power plant |2 × Klimov VK-2500PS-03 turboshaft engines, 1,800 kW (2,400 hp) each for take-off | | | | | |2,000 kW (2,700 hp) emergency rating | +—————–+—————————————————————————————————————————————————————————————————————————————————————————————————————————————————————————————-+ |Speed |280 km/h (170 mph, 150 kn) | +—————–+—————————————————————————————————————————————————————————————————————————————————————————————————————————————————————————————-+ |Accommodation|3 crew and / or 24 troops / 12 stretchers / 4,000 kg (8,818 lb) cargo internally / 5,000 kg (11,023 lb) externally slung | +—————–+—————————————————————————————————————————————————————————————————————————————————————————————————————————————————————————————-+ |Armament |Some variants such as Mi-8AMTSh and Mi-171Sh have disposable stores on six hardpoints, including rockets such as S-8 and gun pods such as UPK-23-250. Some variants such as Mi-171SH-HV and Mi-171SH-VN can be armed with anti-tank guided missiles such as Ataka and precision-guided munitions along with other armaments. Have one or two window-mounted machine guns such as the PK.| | | | | |Other: Drop tanks in hardpoints to increase the range. | +—————–+—————————————————————————————————————————————————————————————————————————————————————————————————————————————————————————————-+# Ka-52 Alligator Heli Ka52 is a Russian single-seat attack helicopter with the distinctive coaxial-contra-rotating rotor system. It has a side fuselage mounted 30 mm cannon.# Cockpit+—————–+——————————————————————————————————————————————————————————————————————————————-+ |First flight |1982 | +—————–+——————————————————————————————————————————————————————————————————————————————-+ |Length |16 m (52 ft 6 in) | +—————–+——————————————————————————————————————————————————————————————————————————————-+ |Height |4.93 m (16 ft 2 in) | +—————–+——————————————————————————————————————————————————————————————————————————————-+ |Ceiling |5,500 m (18,000 ft) | +—————–+——————————————————————————————————————————————————————————————————————————————-+ |Range |545 km (339 mi, 294 nmi) | +—————–+——————————————————————————————————————————————————————————————————————————————-+ |Weight |10,800 kg (23,810 lb) | +—————–+——————————————————————————————————————————————————————————————————————————————-+ |Power plant |2 × Klimov VK-2500 turboshaft engines, 1,800 kW (2,400 shp) each | +—————–+——————————————————————————————————————————————————————————————————————————————-+ |Speed |315 km/h (196 mph, 170 kn) | +—————–+——————————————————————————————————————————————————————————————————————————————-+ |Accommodation|1 crew | +—————–+——————————————————————————————————————————————————————————————————————————————-+ |Armament |Guns: 1× mobile semi-rigid 30 mm Shipunov 2A42 cannon (460 rounds total, dual feeding AP or HE-Frag) | | | | | |Hardpoints: 4 (6 on Ka-52) under-wing hardpoints, plus 2 on wingtips for countermeasures or air-to-air missiles with a capacity of 2,000 kg, with provisions to carry combinations of: | | | | | |Rockets: 80 × 80 mm S-8 rockets and 20 × 122 mm S-13 rocket, | | | | | |Missiles: 2 × APU-6 Missile racks, able to accommodate a total of 12 × 9K121 Vikhr anti-tank missiles | | | | | |Bombs: 4 × 250 kg (550 lb) bombs or 2 × 500 kg (1,100 lb) bombs, | | | | | |Other: 23 mm UPK-23-250 gun pods (240 rounds each), 500 L (130 US gal) external fuel tanks. Reportedly, twin Igla light air-to-air missile launchers under each wingtip countermeasure pod (total 4 missiles).[13] “Iz 305” LMUR AGM/ATGM.| | | | | |Two pods on the wingtips with flare and chaff countermeasure dispensers, 4 UV-26 dispensers each (total 32 chaff/flare cartridges in each pod) | +—————–+——————————————————————————————————————————————————————————————————————————————-+# AH-64AH-64 Apache is an American twin-turboshaft attack helicopter with a tailwheel-type landing gear arrangement and a tandem cockpit for a crew of two. It features a nose-mounted sensor suite for target acquisition and night vision systems.
# Cockpits +—————–+—————————————————————————————————————————————————–+ |First flight |1975 | +—————–+—————————————————————————————————————————————————–+ |Length |58 ft 2 in (17.73 m) | +—————–+—————————————————————————————————————————————————–+ |Height |12 ft 8 in (3.87 m) | +—————–+—————————————————————————————————————————————————–+ |Ceiling |20,000 ft (6,100 m) | +—————–+—————————————————————————————————————————————————–+ |Range |257 nmi (296 mi, 476 km) with Longbow radar mast | +—————–+—————————————————————————————————————————————————–+ |Weight |23,000 lb (10,433 kg) | +—————–+—————————————————————————————————————————————————–+ |Power plant |2 × General Electric T700-GE-701 turboshaft engines, 1,690 shp (1,260 kW) each (upgraded to 1,890 shp (1,409 kW) T700-GE-701C for AH-64A/D from 1990)| +—————–+—————————————————————————————————————————————————–+ |Speed |2,200 km/h | +—————–+—————————————————————————————————————————————————–+ |Accommodation| 2 crew | +—————–+—————————————————————————————————————————————————–+ |Armament |Guns: 1× 30 mm (1.18  in) M230 Chain Gun with 1,200 rounds as part of the Area Weapon Subsystem | | | | | |Hardpoints: Four pylon stations on the stub wings. Longbows also have a station on each wingtip for an AIM-92 Stinger twin missile pack. | | | | | |Rockets: Hydra 70 70 mm, CRV7 70 mm, and APKWS 70 mm air-to-ground rockets | | | | | |Missiles: Typically AGM-114 Hellfire variants; Air-to-Air Stinger (ATAS); AGM-65 Maverick and Spike missiles may also be carried. | +—————–+—————————————————————————————————————————————————–+# MH-65 DolphinThe Eurocopter MH-65 Dolphin is a twin-engined helicopter operated by the United States Coast Guard for medevac-capable search and rescue and armed Airborne Use of Force missions. It is a variant of the French-built Eurocopter AS365 Dauphin.# Cockpit+—————–+——————————————————————–+ |First flight |1980 | +—————–+——————————————————————–+ |Length |11.6 m (38 ft 1 in) | +—————–+——————————————————————–+ |Height |4 m (13 ft 1 in) | +—————–+——————————————————————–+ |Ceiling |5,486 m (17,999 ft) | +—————–+——————————————————————–+ |Range |658 km (409 mi, 355 nmi) | +—————–+——————————————————————–+ |Weight |4,300 kg (9,480 lb) | +—————–+——————————————————————–+ |Power plant |2 × Turbomeca Arriel 2C2-CG turboshaft engines, 636 kW (853 hp) each| +—————–+——————————————————————–+ |Speed |2,200 km/h | +—————–+——————————————————————–+ |Accommodation|2 pilots and 2 crew | +—————–+——————————————————————–+ |Armament |1 x 7.62 mm M240 machine gun | | | | | |1 x Barrett M107 0.50 in (12.70 mm) caliber precision rifle | +—————–+——————————————————————–+#The Bell OH-58 Kiowa is a family of single-engine single-rotor military helicopters used for observation, utility, and direct fire support. It was produced by the American manufacturer Bell Helicopter and is closely related to the Model 206A JetRanger civilian helicopter.
# Cockpit+—————–+—————————————————————————-+ |First flight |1983 | +—————–+—————————————————————————-+ |Length |42 ft 2 in (12.85 m) | +—————–+—————————————————————————-+ |Height |12 ft 10 in (3.93 m) | +—————–+—————————————————————————-+ |Ceiling |15,000 ft (4,575 m) | +—————–+—————————————————————————-+ |Range |161 mi (556 km, 140 nmi) | +—————–+—————————————————————————-+ |Weight |5,500 lb (2,495 kg) | +—————–+—————————————————————————-+ |Power plant |1 × Rolls-Royce T703-AD-700A turboshaft, 650 hp (485 kW) | +—————–+—————————————————————————-+ |Speed |149 mph (240 km/h, 129 kn) | +—————–+—————————————————————————-+ |Accommodation|2 crew | +—————–+—————————————————————————-+ |Armament |Hardpoints: Two pylons , with provisions to carry combinations of: | | | | | |Rockets: 1x LAU-68 rocket launcher with seven 70 mm (2.75”) Hydra 70 rockets| | | | | |Missiles: 2x AGM-114 Hellfire missiles | | | | | |Other: 1x .50 cal (12.7 mm) M3P (or M296) heavy machine gun | +—————–+—————————————————————————-+# CH-53D Sea StallionThe CH-53 Sea Stallion (Sikorsky S-65) is an American family of heavy-lift transport helicopters designed and built by the American manufacturer Sikorsky Aircraft.# Cockpit+—————–+—————————————————————————————————————————————————————————-+ |First flight |1964 | +—————–+—————————————————————————————————————————————————————————-+ |Length |99 ft 0.5 in (30.188 m) | +—————–+—————————————————————————————————————————————————————————-+ |Height |27 ft 9 in (8.46 m) | +—————–+—————————————————————————————————————————————————————————-+ |Ceiling |16,750 ft (5,110 m) | +—————–+—————————————————————————————————————————————————————————-+ |Range |540 nmi (620 mi, 1,000 km) | +—————–+—————————————————————————————————————————————————————————-+ |Weight |42,000 lb (19,051 kg) | +—————–+—————————————————————————————————————————————————————————-+ |Power plant |2 × General Electric T64-GE-413 turboshaft engines, 3,925 shp (2,927 kW) each | +—————–+—————————————————————————————————————————————————————————-+ |Speed |170 kn (200 mph, 310 km/h) | +—————–+—————————————————————————————————————————————————————————-+ |Accommodation|2 pilots, 1 or more loadmasters / crewmen and /or 38 troops (55 in alternate configuration) or 24 stretchers / 8,000 lb (3,600 kg) payload | +—————–+—————————————————————————————————————————————————————————-+ |Armament |Two door mounted .50 BMG GAU-15/A machine guns. Some have a ramp mounted .50 BMG GAU-21 machine gun. | | | | | |German CH-53Gs can mount two 7.62×51mm MG3 machine guns in the side doors, which are to be replaced by two .50 BMG M3M/GAU-21 machines guns in the doors and one on the ramp| +—————–+—————————————————————————————————————————————————————————-+# SH-60 Sea HawkThe Sikorsky SH-60/MH-60 Seahawk is a twin turboshaft engine, multi-mission United States Navy helicopter based on the United States Army UH-60 Black Hawk and a member of the Sikorsky S-70 family. The most significant modifications are the folding main rotor and a hinged tail to reduce its footprint aboard ships.# Cockpit+—————–+———————————————————————————————————————————————————————-+ |First flight |1979 | +—————–+———————————————————————————————————————————————————————-+ |Length |64 ft 8 in (19.71 m) | +—————–+———————————————————————————————————————————————————————-+ |Height |17 ft 2 in (5.23 m) | +—————–+———————————————————————————————————————————————————————-+ |Ceiling |12,000 ft (3,700 m) | +—————–+———————————————————————————————————————————————————————-+ |Range |50 nmi (520 mi, 830 km) | +—————–+———————————————————————————————————————————————————————-+ |Weight |23,000 lb (10,433 kg) | +—————–+———————————————————————————————————————————————————————-+ |Power plant |One Volvo Aero RM12 afterburning turbofan | +—————–+———————————————————————————————————————————————————————-+ |Speed |146 kn (168 mph, 270 km/h) | +—————–+———————————————————————————————————————————————————————-+ |Accommodation|3 -4 crew and/or 5 passengers in cabin, slung load of 6,000 lb (2,700 kg) or internal load of 4,100 lb (1,900 kg) for B, F, and H models / 6,684 lb (3,032 kg) payload| +—————–+———————————————————————————————————————————————————————-+ |Armament |Up to two Mark 46 torpedoes or Mk 50 or Mk-54s or two 120 U.S. gal (454 L) fuel tanks for SH-60B and HH-60R and MH-60R | | | | | |AGM-114 Hellfire missile, 4 Hellfire missiles for SH-60B and HH-60H and MH-60R, 8 Hellfire missiles for MH-60S Block III. | | | | | |AGM-119 Penguin missile (being phased out), | | | | | |APKWS Advanced Precision Kill Weapon System, | | | | | |M60 machine gun or, M240 machine gun or GAU-16/A machine gun or GAU-17/A Minigun | | | | | |Rapid Airborne Mine Clearance System (RAMICS) using Mk 44 Mod 0 30 mm Cannon | +—————–+———————————————————————————————————————————————————————-+# MerlinThe AgustaWestland AW101 is a medium-lift helicopter in military and civil use. First flown in 1987, it was developed by a joint venture between Westland Helicopters in the United Kingdom and Agusta in Italy in response to national requirements for a modern naval utility helicopter.# Cockpit+—————–+————————————————————————————————————————————————–+ |First flight |1987 | +—————–+————————————————————————————————————————————————–+ |Length |19.53 m (64 ft 1 in) | +—————–+————————————————————————————————————————————————–+ |Height |6.62 m (21 ft 9 in) | +—————–+————————————————————————————————————————————————–+ |Ceiling |4,575 m (15,010 ft) | +—————–+————————————————————————————————————————————————–+ |Range |1,389 km (863 mi, 750 nmi) | +—————–+————————————————————————————————————————————————–+ |Weight |14,600 kg (32,187 lb) | +—————–+————————————————————————————————————————————————–+ |Power plant |3 × Rolls-Royce Turbomeca RTM322-01 turboshaft engines, 1,566 kW (2,100 hp) each (take-off power) | +—————–+————————————————————————————————————————————————–+ |Speed |309 km/h (192 mph, 167 kn) | +—————–+————————————————————————————————————————————————–+ |Accommodation|3 -4 crew and/or 26 troops (38 passengers) or 5 tonnes of payload or 4 stretchers (with sonar array removed) for Merlin HM1; | | | | | |30 seated troops or 45 standing fully equipped combat troops, or 3,050 kg (6,724 lb) of internal payload, 5,520 kg (12,169 lb) of external payload| +—————–+————————————————————————————————————————————————–+ |Armament |Bombs: 4× Sting Ray homing torpedoes or Mk 11 depth charges | +—————–+————————————————————————————————————————————————–+# NH90The NHIndustries NH90 is a medium-sized, twin-engine, multi-role military helicopter. It was developed in response to NATO requirements for a battlefield helicopter which would also be capable of being operated in naval environments.# Cockpit+—————–+—————————————————————————————————————————————————————+ |First flight |1995 | +—————–+—————————————————————————————————————————————————————+ |Length |16.13 m (52 ft 11 in) | +—————–+—————————————————————————————————————————————————————+ |Height |5.31 m (17.42 ft ) | +—————–+—————————————————————————————————————————————————————+ |Ceiling |6,000 m (20,000 ft) | +—————–+—————————————————————————————————————————————————————+ |Range |00 km (500 mi, 430 nmi) | +—————–+—————————————————————————————————————————————————————+ |Weight |10,600 kg (23,369 lb) | +—————–+—————————————————————————————————————————————————————+ |Power plant |2 × General Electric CT7-8E turboshaft engines, 1,845 kW (2,474 hp) each (option) | +—————–+—————————————————————————————————————————————————————+ |Speed |300 km/h (190 mph, 160 kn) | +—————–+—————————————————————————————————————————————————————+ |Accommodation|2 flight crew + loadmaster / sensor operator and/or 20 seated troops; or 12 medevac stretchers; or 2 NATO pallets; or 4,200 kg (9,259 lb) external slung load| +—————–+—————————————————————————————————————————————————————+ |Armament |Guns: 2 door guns | | | | | |Missiles: anti-submarine and/or air to surface missiles (NFH version) | +—————–+—————————————————————————————————————————————————————+# V-22 V-22 Osprey is an American multi-mission, tiltrotor military aircraft with both vertical takeoff and landing and short takeoff and landing capabilities. It is designed to combine the functionality of a conventional helicopter with the long-range, high-speed cruise performance of a turboprop aircraft.# Cockpit+—————–+——————————————————————————————————————————-+ |First flight |1989 | +—————–+——————————————————————————————————————————-+ |Length |57 ft 4 in (17.48 m) | +—————–+——————————————————————————————————————————-+ |Height |22 ft 1 in (6.73 m) engine nacelles vertical | | | | | |17 ft 7.8 in (5 m) to top of tailfins | +—————–+——————————————————————————————————————————-+ |Ceiling |25,000 ft (7,600 m) | +—————–+——————————————————————————————————————————-+ |Range |879 nmi (1,012 mi, 1,628 km) | +—————–+——————————————————————————————————————————-+ |Weight |55,000 lb (24,948 kg) | +—————–+——————————————————————————————————————————-+ |Power plant |2 × Rolls-Royce T406-AD-400 turboprop/turboshaft engines, 6,150 hp (4,590 kW) each maximum at 15,000 rpm at sea level | +—————–+——————————————————————————————————————————-+ |Speed |305 kn (565 km/h; 351 mph) at 15,000 ft (4,600 m) | | | | | |275 kn (316 mph, 509 km/h) | +—————–+——————————————————————————————————————————-+ |Accommodation|3–4 (pilot, copilot and 1 or 2 flight engineers/crew chiefs/loadmasters/gunners) | | | | | |and/ or 24 troops (seated), 32 troops (floor loaded), or | | | | | |20,000 lb (9,070 kg) of internal cargo, or up to 15,000 lb (6,800 kg) of external cargo (dual hook) | | | | | |1× M1161 Growler light internally transportable ground vehicle | +—————–+——————————————————————————————————————————-+ |Armament |× 7.62 mm (.308 in) M240 machine gun or .50 in (12.7 mm) M2 Browning machine gun on ramp, removable | | | | | |1× 7.62 mm (.308 in) GAU-17 minigun, belly-mounted, retractable, video remote control in the Remote Guardian System [optional]| +—————–+——————————————————————————————————————————-+# AW119MMission flexibility is crucial to military helicopter operations. The AW119M provides exceptional multi-mission performance, allied with the ability to operate in challenging environments, day and night. The light single-engine AW119M is the military version of the AW119Kx and is the only helicopter in its class with the inherent safety provided by redundant main systems. With spacious reconfigurable cabin offers more room than any other single-engine helicopter and can be reconfigured rapidly to satisfy a large variety of roles. Large sliding doors on both sides of the helicopter enable fast access for troops, equipment or a stretcher. Up to two door-mounted machine guns can be installed on the aircraft.# Cockpit+—————–+————————————————————————+ |First flight |1995 | +—————–+————————————————————————+ |Length |12.92 m (42 ft 5 in) | +—————–+————————————————————————+ |Height |3.60 m (11 ft 10 in) | +—————–+————————————————————————+ |Ceiling |4,572 m (15,000 ft) | +—————–+————————————————————————+ |Range |954 km (593 mi, 515 nmi) | +—————–+————————————————————————+ |Weight |2,850 kg (6,283 lb) | +—————–+————————————————————————+ |Power plant |1 × Pratt & Whitney Canada PT6B-37A turboshaft engine, 747 kW (1,002 hp)| +—————–+————————————————————————+ |Speed |244 km/h (152 mph, 132 kn) | +—————–+————————————————————————+ |Accommodation|1 or 2 crew | | | | | |6-7 passengers or 1,400 kg (3,086 lb) sling load | +—————–+————————————————————————+ |Armament |
| +—————–+————————————————————————+# Z-10The CAIC Z-10 is a Chinese medium attack helicopter developed for the People’s Liberation Army Ground Force. It is designed primarily for anti-tank warfare missions but has secondary air-to-air combat capability as well.# Cockpit+—————–+——————————————————————————————–+ |First flight |2003 | +—————–+——————————————————————————————–+ |Length |14.15 m (46 ft 5 in | +—————–+——————————————————————————————–+ |Height |3.85 m (12 ft 8 in) | +—————–+——————————————————————————————–+ |Ceiling |6,400 m (21,000 ft) | +—————–+——————————————————————————————–+ |Range |800 km (500 mi, 430 nmi) | +—————–+——————————————————————————————–+ |Weight |7,000 kg (15,432 lb) | +—————–+——————————————————————————————–+ |Power plant |2 × WZ-9 turboshaft engines, 930–957 kW (1,247–1,283 hp) each | +—————–+——————————————————————————————–+ |Speed |2,200 km/h | +—————–+——————————————————————————————–+ |Accommodation|2 crew | +—————–+——————————————————————————————–+ |Armament |Guns: 1x 23 mm (0.906 in) revolver gun or 1x 25 mm (0.984 in) M242 Bushmaster chain gun copy| | | | | |Hardpoints: 4 with a capacity of 1,500 kg (3,307 lb) useful load | | | | | |Rockets: 57 mm (2.244 in) or 90 mm (3.543 in) unguided rocket pods | | | | | |Missiles: For each hardpoint: | | | | | |4× HJ-8, HJ-9 laser-guided air-to-surface missiles | | | | | |4× AKD-10 (BA-7) laser-guided air-to-surface missiles | | | | | |4× AKD-9 (BA-9) laser-guided air-to-surface missiles | | | | | |4× AKD-21 (BA-21) millimeter-wave air-to-surface missiles | | | | | |4× AG300M or AG300L laser-guided air-to-surface missiles | | | | | |4× CM-502KG or CM-502V NLOS air-to-surface missiles | | | | | |2× CM-501GA NLOS air-to-surface missiles | | | | | |1× CM-501XA loitering munition | | | | | |4× TY-90 air-to-air missiles | +—————–+——————————————————————————————–+# Eurocopter TigerThe Eurocopter Tiger is a four-blade, twin-engine attack helicopter which first entered service in 2003. It is manufactured by Airbus Helicopters, which arose from the merger of Aérospatiale’s and DASA’s respective helicopter divisions. Airbus Helicopters designates it as the EC665.# Cockpit+—————–+———————————————————————–+ |First flight |1991 | +—————–+———————————————————————–+ |Length |14.08 m (46 ft 2 in) | +—————–+———————————————————————–+ |Height |3.83 m (12 ft 7 in) | +—————–+———————————————————————–+ |Ceiling |4,000 m (13,000 ft) | +—————–+———————————————————————–+ |Range |800 km (500 mi, 430 nmi) | +—————–+———————————————————————–+ |Weight |6,000 kg (13,228 lb) | +—————–+———————————————————————–+ |Power plant |2 × MTR MTR390 turboshaft engines, 972 kW (1,303 shp) each | +—————–+———————————————————————–+ |Speed |2,200 km/h | +—————–+———————————————————————–+ |Accommodation|2 crew | +—————–+———————————————————————–+ |Armament |Guns: | | | | | |1× 30 mm (1.18 in) GIAT 30 cannon in chin turret, with up to 450 rounds| +—————–+———————————————————————–+# H145MH145M is the wide range of available optional mission equipment packages that can be rapidly installed and removed, based on the requirements of the mission. Within minutes, the aircraft can be reconfigured from troop transport with seats to a search and rescue mission with rescue hoist and stretchers, or to an armed helicopter with a set of weapons and ballistic protection.

# Cockpit+—————–+——————————————————————————+ |First flight |1988 | +—————–+——————————————————————————+ |Length |13.03 m (42 ft 9 in) | +—————–+——————————————————————————+ |Height |3.45 m (11 ft 4 in) | +—————–+——————————————————————————+ |Ceiling |5,240 m (17,190 ft) | +—————–+——————————————————————————+ |Range |680 km (420 mi, 370 nmi) | +—————–+——————————————————————————+ |Weight |3,585 kg (7,904 lb) | +—————–+——————————————————————————+ |Power plant |2 × Turbomeca Arriel 1E2 turboshaft engines, 550 kW (740 hp) each for take-off| +—————–+——————————————————————————+ |Speed |268 km/h (167 mph, 145 kn) | +—————–+——————————————————————————+ |Accommodation|2 crew | | | | | |and/or 9 pax / 1,793 kg (3,953 lb) payload | +—————–+——————————————————————————+ |Armament |Cannon 20 mm | | | | | |Machine gun 12.7 mm | | | | | |Rocket 68 and 70 mm | | | | | |Guided: | | | | | |Laser-guided rocket | | | | | |Air-to-ground missile | | | | | |Air-to-air missile (with growth potential) | +—————–+——————————————————————————+# MBB Bo-105The Bo-105 light utility helicopter was developed by Messerschmitt-Bolkow-Blohm (MBB) of West Germany in the early 70s. Originally it was intended for civil market, but due to its high maneuverability and excellent climb rate a military version has been created with a Widened cabin to seat 7. The Bo-105 was license-produced in Indonesia, Philippines, South Korea and Spain. This helicopter has been widely exported even despite high unit cost. It remains in service with at least 20 countries around the world. # Cockpit+—————–+————————————————————–+ |First flight |1967 | +—————–+————————————————————–+ |Length |11.86 m (38 ft 11 in) | +—————–+————————————————————–+ |Height |3.00 m (9 ft 10 in) | +—————–+————————————————————–+ |Ceiling |5,200 m (17,000 ft) | +—————–+————————————————————–+ |Range |57 km (408 mi, 355 nmi) | +—————–+————————————————————–+ |Weight |2,500 kg (5,512 lb) | +—————–+————————————————————–+ |Power plant |2 × Allison 250-C20B turboshaft engines, 310 kW (420 shp) each| +—————–+————————————————————–+ |Speed |270 km/h (170 mph, 150 kn) | +—————–+————————————————————–+ |Accommodation|1 or 2 crew | | | | | |3 or 4 passengers | +—————–+————————————————————–+ |Armament |Missiles: 6x Euromissile HOT (Bo 105 P) or 8x BGM-71 TOW | +—————–+————————————————————–+# Changhe Z-11The Changhe Z-11 is a light utility helicopter developed by Changhe Aircraft Industries Corporation. According to the Changhe Aircraft Industries Corporation website, it is claimed to be the first indigenously-designed helicopter in China. However, it is largely based on the Eurocopter AS350 Écureuil.# Cockpit+—————–+——————————————————————————-+ |First flight |1994 | +—————–+——————————————————————————-+ |Length |11.24 m (36 ft 11 in) fuselage | | | | | |13.01 m (43 ft) with rotors turning | +—————–+——————————————————————————-+ |Height |3.14 m (10 ft 4 in) to top of rotor hub | +—————–+——————————————————————————-+ |Ceiling |5,270 m (17,290 ft) | +—————–+——————————————————————————-+ |Range |661 km (411 mi, 357 nmi | +—————–+——————————————————————————-+ |Weight |2,250 kg (4,960 lb) | +—————–+——————————————————————————-+ |Power plant |1 × Liming WZ-8 turboshaft engine, 510 kW (680 hp) for take-off | +—————–+——————————————————————————-+ |Speed |258 km/h (160 mph, 139 kn) max at 1,000 m (3,281 ft) | +—————–+——————————————————————————-+ |Accommodation|1 crew -6 Capacity | +—————–+——————————————————————————-+ |Armament |Guns: | | | | | |1× 7.62 mm (0.300 in) pintle mounted CS/LM12 six-barreled minigun | | | | | |1× 40 mm (1.575 in) pintle mounted LG3 automatic grenade launcher | | | | | |1× 23 mm (0.906 in) pylon mounted gun pod | | | | | |Hardpoints: 16 | | | | | |Rockets: Up to 2× 57 mm (2.244 in) unguided rocket pods | | | | | |Missiles: | | | | | |Up to 4× TL-2, AG-300/M, CM-502KG air-to-surface anti-tank / anti-ship missiles| | | | | |Up to 8× HJ-8, HJ-10 air-to-surface missiles | | | | | |Up to 8× TY-90 air-to-air missiles | | | | | |Up to 8× SW-6 air deployable tactical unmanned aerial vehicle (UAV) | | | | | |Bombs: Up to 4× FT-9 or YZ-212D laser-guided precision bombs | +—————–+——————————————————————————-+

# Mi 28The Mil Mi-28 is a Russian all-weather, day-night, military tandem, two-seat anti-armor attack helicopter. It is an attack helicopter with no intended secondary transport capability, better optimized than the Mil Mi-24 gunship for the role.# Cockpit

+—————–+———————————————————————————————————————————————————————+ |First flight |1982 | +—————–+———————————————————————————————————————————————————————+ |Length |17.01 m (55 ft 10 in) | +—————–+———————————————————————————————————————————————————————+ |Height |3.82 m (12 ft 6 in) | +—————–+———————————————————————————————————————————————————————+ |Ceiling |5,700 m (18,700 ft) | +—————–+———————————————————————————————————————————————————————+ |Range |435 km (270 mi, 235 nmi) | +—————–+———————————————————————————————————————————————————————+ |Weight |11,500 kg (25,353 lb) | +—————–+———————————————————————————————————————————————————————+ |Power plant |2 × Klimov TV3-117 turboshaft engines, 1,636 kW (2,194 hp) each | +—————–+———————————————————————————————————————————————————————+ |Speed |20 km/h (200 mph, 170 kn) | +—————–+———————————————————————————————————————————————————————+ |Accommodation|2 crew | +—————–+———————————————————————————————————————————————————————+ |Armament |Guns: 1× chin-mounted 30 mm Shipunov 2A42 cannon with 250 rounds (±110° horizontal fire) | | | | | |Hardpoints: Two pylons under each stub wing to mount bombs, rockets, missiles, and gun pods. Main armament configurations include: | | | | | |16 Ataka-V anti-tank missiles and 40 S-8 rockets, Or | | | | | |16 Ataka-V anti-tank missiles, and 10 S-13 rocket, Or | | | | | |16 Ataka-V anti-tank missiles, and two 23 mm UPK-23-250 gun pods each containing a GSh-23L with 250 rounds. | | | | | |Other ordnance: 9K121 Vikhr, and 9M123 Khrizantema anti-tank missiles, “Iz 305” LMUR AGM/ATGM, 8 Igla-V and Vympel R-73 air-to-air missiles, 2 KMGU-2 mine dispensers| +—————–+———————————————————————————————————————————————————————+
# Mi 24# Cockpit +—————–+—————————————————————————————————————–+ |First flight |1969 | +—————–+—————————————————————————————————————–+ |Length |17.5 m (57 ft 5 in) | +—————–+—————————————————————————————————————–+ |Height |6.5 m (21 ft 4 in) | +—————–+—————————————————————————————————————–+ |Ceiling |4,900 m (16,100 ft) | +—————–+—————————————————————————————————————–+ |Range |450 km (280 mi, 240 nmi) | +—————–+—————————————————————————————————————–+ |Weight |12,000 kg (26,455 lb) | +—————–+—————————————————————————————————————–+ |Power plant |2 × Isotov TV3-117 turboshaft engines, 1,600 kW (2,200 shp) each | +—————–+—————————————————————————————————————–+ |Speed |335 km/h (208 mph, 181 kn) | +—————–+—————————————————————————————————————–+ |Accommodation|2-3 pilot | | | | | |8 troops / 4 stretchers / 2,400 kg (5,291 lb) cargo on an external sling | +—————–+—————————————————————————————————————–+ |Armament |Internal guns: | | | | | |flexible 12.7 mm Yakushev-Borzov Yak-B Gatling gun on most variants. Maximum of 1,470 rounds of ammunition. | | | | | |fixed twin-barrel GSh-30K autocannon on the Mi-24P. 250 rounds of ammunition. | | | | | |flexible twin-barrel GSh-23L autocannon on the Mi-24VP and Mi-24VM. 450 rounds of ammunition. | | | | | |flexible GIAT dual feed 20mm (M693) autocannon on Mi-24 SuperHind Mk.II/III/IV/V. 320 rounds of ammunition. | | | | | |PKB passenger compartment window mounted machine guns | | | | | |
| | | | | |External stores: | | | | | |Total payload is 1,500 kg of external stores. | | | | | |Inner hardpoints can carry at least 500 kg | | | | | |Outer hardpoints can carry up to 250 kg | | | | | |Wing-tip pylons can only carry the 9M17 Phalanga (in the Mi-24A-D) or the 9K114 Shturm complex (in the Mi-24V-F).| | | | | |
| | | | | |Bomb-load: | | | | | |Bombs within weight range (presumably ZAB, FAB, RBK, ODAB etc.), up to 500 kg. | | | | | |MBD multiple ejector racks (presumably MBD-4 with 4 × FAB-100) | | | | | |KGMU2V submunition/mine dispenser pods | | | | | |First-generation armament (standard production Mi-24D) | | | | | |GUV-8700 gunpod (with a 12.7 mm Yak-B + 2 × 7.62 mm GShG-7.62 mm combination or one 30 mm AGS-17) | | | | | |UB-16 S-5 rocket launchers | | | | | |UB-32 S-5 rocket launchers | | | | | |S-24 240 mm rocket | | | | | |9M17 Fleyta (a pair on each wingtip pylon) | | | | | |
| | | | | |Second-generation armament (Mi-24V, Mi-24P and most upgraded Mi-24D) | | | | | |UPK-23-250 gunpod carrying the GSh-23L | | | | | |B-8V20 a lightweight long tubed helicopter version of the S-8 rocket launcher | | | | | |9K114 Shturm in pairs on the outer and wingtip pylons | +—————–+—————————————————————————————————————–+


# IAIO Toufan# Cockpit +—————–+—————————————————————————————————+ |First flight |2010 | +—————–+—————————————————————————————————+ |Length |53 ft (16 m) | +—————–+—————————————————————————————————+ |Height |13 ft 6 in (4.11 m) | +—————–+—————————————————————————————————+ |Ceiling |11,400 ft (3,500 m) | +—————–+—————————————————————————————————+ |Range |310 nmi (360 mi, 570 km) | +—————–+—————————————————————————————————+ |Weight |9,500 lb (4,309 kg) | +—————–+—————————————————————————————————+ |Power plant |Turboshaft engine | +—————–+—————————————————————————————————+ |Speed |190 kn (220 mph, 350 km/h) | +—————–+—————————————————————————————————+ |Accommodation| 2 crew | +—————–+—————————————————————————————————+ |Armament |2 × 7.62 mm (0.308 in) multi-barrel Miniguns | | | | | |2.75 in (70 mm) rockets – 7 rockets mounted in the M158 launcher or 19 rockets in the M200 launcher| +—————–+—————————————————————————————————+
# Kazan Ansat# Cockpit+—————–+—————————————————————————+ |First flight |1999 | +—————–+—————————————————————————+ |Length |13.76 m (45 ft 2 in) | +—————–+—————————————————————————+ |Height |3.4 m (11 ft 2 in) | +—————–+—————————————————————————+ |Ceiling |5,500 m (18,000 ft) | +—————–+—————————————————————————+ |Range |505 km (314 mi, 273 nmi) | +—————–+—————————————————————————+ |Weight |3,600 kg (7,937 lb) | +—————–+—————————————————————————+ |Power plant |2 × Pratt & Whitney Canada PW207K turboshaft engines, 470 kW (630 shp) each| +—————–+—————————————————————————+ |Speed |275 km/h (171 mph, 148 kn) | +—————–+—————————————————————————+ |Accommodation|1 or 2 crew | | | | | |7–8 passengers | | | | | |2 stretchers and 3 attendants 1,235 kg (2,723 lb) internal | +—————–+—————————————————————————+ |Armament |
| +—————–+—————————————————————————+

# Mi-38# Cockpit +—————–+———————————————————————————————+ |First flight |2003 | +—————–+———————————————————————————————+ |Length |20.282 m (66 ft 7 in) | +—————–+———————————————————————————————+ |Height |6.992 m (22 ft 11 in) | +—————–+———————————————————————————————+ |Ceiling |6,300 m (20,700 ft) | +—————–+———————————————————————————————+ |Range |880 km (550 mi, 480 nmi) | +—————–+———————————————————————————————+ |Weight |15,600 kg (34,392 lb) | +—————–+———————————————————————————————+ |Power plant |2 × Klimov TV7-117V turboshaft engines, 2,100 kW (2,800 hp) each | +—————–+———————————————————————————————+ |Speed |300 km/h (190 mph, 160 kn) | +—————–+———————————————————————————————+ |Accommodation|2 crew | | | | | |30 troops max / 6,000 kg (13,000 lb) internal payload / 7,000 kg (15,000 lb) external payload| +—————–+———————————————————————————————+ |Armament |
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# Battlespace Progression Tree For HelicoptersNATO
Helicopters Nato.docx
CSTO
Helicopters CSTO.docx