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 UH-1Y Venom vs. UH-60 Blackhawk

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UH-1Y or UH-60
UH-1Y Venom [Modernized Huey]
60%
 60% [ 3 ]
UH-60 Blackhawk
40%
 40% [ 2 ]
Total Votes : 5
 

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PostSubject: UH-1Y Venom vs. UH-60 Blackhawk   Sat Jun 05, 2010 10:17 am


( A Marines UH-1Y Venom hovering over the Atlantic )


( An Army Blackhawk doing a lower-level air support mission in Afghanistan )
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PostSubject: Re: UH-1Y Venom vs. UH-60 Blackhawk   Sat Jun 05, 2010 10:28 am

The Venom is known to fly missions with AH-1Z Vipers in Iraq and Afghanistan. The Marines just don't want to get rid of the Huey, so they redo it. Four rotors. Known for it's ability to do air support, and utility operations. And of course, they update the AH-1W Super Cobra, to the AH-1Z Viper. The Marines don't want the apache. They've got their signiture bird, so does the army. The Army uses the Blackhawk and the Apache, the Marines use the Venom and the Viper. Notice how you can't find a UH-1Y that says ARMY on the side of it.


This is the perfect example. You always see a Venom with a Viper. That's what I call, COMBAT AIR PATROL.





The UH-1Y variant modernizes the UH-1 design. Its most noticeable upgrade, as compared to previous variants, is a four-bladed, all-composite rotor system designed to withstand ballistics up to 23 mm. A 21-inch (530 mm) insert just forward of the main door has been installed for more capacity. The UH-1Y has upgraded engines and transmission, 170% increased payload over UH-1N, almost 50% greater range and maximum speed, a digital cockpit with flat panel multifunctional displays, and an 84% parts commonality with the AH-1Z.

On 8 August 2008, the Marine Corps certified the UH-1Y as operationally capable and was deployed for the first time in January 2009 as part of the aviation combat element of the 13th Marine Expeditionary Unit. The Marine Corps plans to eventually buy 123 of the Y-model Hueys to replace their inventory of N-models, with delivery of all aircraft to be complete by 2016.

The only operator of the UH-1Y is the United States Marine Corps.

General characteristics

Crew: One or two pilots, plus crew chief, other crew members as mission requires
Capacity: 6,660 lb (3,020 kg) including up to 10 crashworthy passenger seats, 6 litters or equivalent cargo[23]
Length: 58 ft 4 in (17.78 m)
Rotor diameter: 48 ft 10 in (14.88 m)
Height: 14 ft 7 in (4.5 m)
Disc area: 1,808 ft² (168.0 m²)
Empty weight: 11,840 lb (5,370 kg)
Useful load: 6,660 lb (3,020 kg)
Max takeoff weight: 18,500 lb (8,390 kg)
Powerplant: 2× General Electric T700-GE-401C turboshaft, 1,828 shp for 2.5 min; 1,546 shp continuous (1,360 kW for 2.5 min; 1,150 kW continuous) each
Performance

Never exceed speed: 198 kn (227 mph, 366 km/h)
Maximum speed: 164 knots (189 mph, 304 km/h) for 30 minutes
Cruise speed: 158 kt, 182 mph, 293 km/h (long range cruise (LRC): 135 kn, 155 mph, 250 km/h)
Range: 130 nmi (150 mi, 241 km) with 2,182 lb, 990 kg payload
Service ceiling: 20,000+ ft (6,100+ m)
Rate of climb: 2,520 ft/min (12.8 m/s)
Armament


2 external stations for 70 mm (2.75 in) Hydra 70 rockets
2 pintle mounts for 7.62 mm M240D machine guns, .50 BMG GAU-16/A machine guns, or 7.62 mm GAU-17/A Gatling guns


The AH-1Z Viper

The AH-1Z incorporates new rotor technology with upgraded military avionics, weapons systems, and electro-optical sensors in an integrated weapons platform. It has improved survivability and can find targets at longer ranges and attack them with precision weapons.


An AH-1Z at an air show displaying four-blade rotors and longer stub wings.The AH-1Z's new bearingless, hingeless rotor system has 75% fewer parts than that of four-bladed articulated systems. The blades are made of composites, which have an increased ballistic survivability, and there is a semiautomatic folding system for stowage aboard Amphibious assault ships. Its two redesigned wing stubs are longer, with each adding a wing-tip station for a missile such as the AIM-9 Sidewinder. Each wing has two other stations for 2.75-inch (70 mm) Hydra 70 rocket pods, or AGM-114 Hellfire quad missile launchers. The Longbow radar can also be mounted on a wing tip station.

The Z-model's integrated avionics system (IAS) has been developed by Northrop Grumman. The system include two mission computers and an automatic flight control system. Each crew station has two 8x6-inch multifunction liquid crystal displays (LCD) and one 4.2x4.2-inch dual function LCD display. The communications suite combines a US Navy RT-1824 integrated radio, UHF/VHF, COMSEC and modem in a single unit. The navigation suite includes an embedded GPS inertial navigation system (EGI), a digital map system and a low-airspeed air data subsystem, which allows weapons delivery when hovering.

The crew are equipped with the Thales "Top Owl" helmet-mounted sight and display system. The Top Owl has a 24-hour day/night capability and a binocular display with a 40° field of view. Its visor projection provides forward looking infrared (FLIR) or video imagery. The AH-1Z has survivability equipment including the Hover Infared Suppression System (HIRSS) to cover engine exhausts, countermeasure dispensers, radar warning, incoming/on-way missile warning and on-fuselage laserspot warning systems.

The Lockheed Martin target sight system (TSS) incorporates a third-generation FLIR sensor. The TSS provides target sighting in day, night or adverse weather conditions. The system has various view modes and can track with FLIR or by TV.

The only operators of the AH-1Z are the United States Marine Corps.

General characteristics

Crew: 2: pilot, CPG (co-pilot/gunner)
Capacity: 6,661 lb (3,021 kg)
Length: 58 ft 3 in (17.8 m)
Rotor diameter: 48 ft (14.6 m)
Height: 14 ft 4 in (4.37 m)
Disc area: 1,808 ft² (168.0 m²)
Empty weight: 12,300 lb (5,580 kg)
Useful load: 5,764 lb (2,620 kg)
Max takeoff weight: 18,500 lb (8,390 kg)
Powerplant: 2× General Electric T700-GE-401C turboshaft, 1,800 shp (1,340 kW) each
Rotor systems: 4 blades on main rotor, 4 blades on tail rotor
Performance

Never exceed speed: 222 knots (255 mph, 411 km/h)
Cruise speed: 160 kn (184 mph, 296 km/h)
Range: 370 nmi (426 mi, 685 km)
Combat radius: 125 nmi (144 mi, 231 km) with 2,500 lb (1,130 kg) payload
Service ceiling: 20,000+ ft (6,100+ m)
Rate of climb: 2,790 ft/min (14.2 m/s)
Armament


Guns: 1 x 3-barreled 20 mm M197 Gatling gun in the A/A49E-7 turret (750 round ammo capacity)
Hardpoints: Up to 6 pylon stations on stub wing
Rockets: 2.75 in (70 mm) Hydra 70 rockets - Mounted in LAU-68C/A (7 shot) or LAU-61D/A (19 shot) launchers
Missiles:

AIM-9 Sidewinder air-to-air missiles - 1 mounted on each wing tip station (total of 2)
AGM-114 Hellfire air-to-surface missiles - Up to 16 missiles mounted in four 4-round M272 missile launchers, two on each wing
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