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MD 500 Defender American Light Multi-Role Helicopter

MD 500 Defender

Utility Helicopter
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Basic Information
Name
MD 500 Defender American Light Multi-Role Helicopter
Designation
MD 500 Defender
Alternate Designation
MD 500 Defender; 500MD Defender
Equipment Type
Utility Helicopter
Manufacturer
Hughes Helicopters McDonnell Douglas Helicopter Systems MD Helicopters
Date of Introduction
1976
Description

The McDonnell Douglas Helicopter Systems MD 500 Defender is a light multi-role military helicopter based on the MD 500 light utility helicopter and OH-6 Cayuse Light Observation Helicopter. The Defender 500 foreign military sales helicopter is offered with either a four- or five-blade main rotor, depending on the model, with a weapons platform mounted on the lower rear body. This light utility commercial helicopter could seat five passengers in comfort, and is used mainly by the military, being very flexible and offering good all round capabilities. Other missions include: direct air support, antitank, reconnaissance, observation, and light utility. A single engine is mounted inside the body with air intakes on top of the cabin and a black hole exhaust. The fuselage is teardrop-shaped a features a round, glassed-in cockpit and landing skids. External stores are mounted on weapons racks on each side of the fuselage. Each rack has one hardpoint. The tail fin is boomerang-shaped, swept-back, and tapered. The tail flats are back-tapered with small fins attached to the tips, with the flats high-mounted on the fin forming a T. The rotor is mounted on the lower left of the tail boom. The successful Hughes 500/MD 500 series began life in response to a U.S. Army requirement for a Light Observation Helicopter (LOH). Hughes' Model 369 won the contest against competition from Bell and Hiller. The subsequent OH-6 Cayuse first flew in February 1963. The 500 series design features shock-absorbing landing skid struts, a turboshaft engine mounted at a 45-degree angle toward the rear of the cabin pod, a fuel tank cell under the floor and the battery in the nose. The engine exhaust port is located at the end of the cabin pod underneath the tailboom. It has a short-diameter main rotor system and a short tail, giving it agile control response and is less susceptible to weather-cocking. Hughes won the U.S. Army's LOH contest with its OH-6 helicopter by submitting a very low and aggressive price per airframe (without an engine). Due to rising prices, the U.S. Army later re-opened the contest, where Hughes offered the machine at a more realistic price, but was undercut by the redesigned Bell OH-58 Kiowa (military JetRanger). OH-6 helicopters were still ordered by the U.S. Army, though at a much reduced number. Prior to the OH-6's first flight, Hughes announced it was developing a civil version, to be marketed as the Hughes 500, available in basic five- and seven-seat configurations.[3] A utility version with a more powerful engine was offered as the 500U (later called the 500C). The improved Hughes 500D became the primary model in 1976, with a more powerful engine, a T-tail, and a new five-blade main rotor; a four-blade tail rotor was optional. The 500D was replaced by the 500E from 1982 with a pointed nose and various interior improvements, such as greater head- and legroom. The 530F was a more powerful version of the 500E optimized for hot and high work. McDonnell Douglas acquired Hughes Helicopters in January 1984, and from August 1985 the 500E and 530F were built as the MD 500E and MD 530F Lifter. Following the 1997 Boeing-McDonnell Douglas merger, Boeing sold the former MD civil helicopter lines to MD Helicopters in early 1999. Military variants are marketed under the MD 500 Defender name.

Air & Air Defense Specifications
Crew 2
Endurance 2.80 hrs
Rotor Diameter 8.10 m
Variants
500D Scout Defender Armed reconnaissance version
500M Defender Military export version of the 500 and 500C, built under license by Kawasaki in Japan (as the OH-6J)[7] and Breda Nardi in Italy.
500M/ASW Defender Export version for the Spanish Navy.
NH-500M Defender Italian-built version of the 500M Defender. Licensed by Breda Nardi before merge with Agusta.
500MD Defender Military version of the 500D. Korean Air's aerospace division from 1976 to 1984 with 200 choppers made. 50 were armed with TOW anti-tank missiles and 150 choppers used for transportation and support duties.
500MD/ASW Defender Maritime version of the 500MD Defender.
500MD/TOW Defender Anti-tank version of the 500MD Defender, armed with TOW anti-tank missiles.
500MD/MMS-TOW Defender Anti-tank version, fitted with a mast-mounted sight, armed with TOW anti-tank missiles.
500MD Quiet Advanced Scout Defender Fitted with noise suppression equipment.
500MD Defender II Improved version.
500MG Defender Military version of the 500E.
520MG Defender Philippine military version. Special Forces version. Modified 500MG Defender that carry .50 caliber machine guns and 7-tube rocket pods and operates as a light attack aircraft.
520MK Black Tiger South Korean-built military version, built by Korean Air Aerospace Division[
530MG Defender Military version of the 530F.
MD530 Nightfox Night attack version.
MD530MG Paramilitary Defender Police or border patrol version.
MD540F Upgraded MD530F, incorporating a 6-bladed, fully articulated rotor blade system made of composite material, a more rugged landing skid for heavier take-off and landing weights, a fully integrated digital glass cockpit with multi-function color displays and a pilot Helmet Display and Tracking System (HDTS), which couples together a targeting FLIR and laser designator.
MD530G Designed based on the MD 530F airframe and is engineered with advanced technology to deliver enhanced combat capabilities.
System
Alternative Designation MD 500 Defender; 500MD Defender
Type Light multi-role military helicopter
Manufacturer Hughes Helicopters McDonnell Douglas Helicopter Systems MD Helicopters
In Service 1976-Present
Crew 2 (pilot, co-pilot) ea
Passengers + 6 troops
Blades, Main Rotor five-blade main rotor, many with four-blade anti-torque rotor
Blades, Tail Rotor 2 ea
Number of Engines 1 ea
Day/Night Capable Yes, depending on additional equipment added
All Weather Capable Yes, depending on additional equipment added
Takeoff or Landing Limitations INA
Number of Hard Points 2 ea
Landing Skid The parallel-skid landing gear has internal oleo-pneumatic shock absorbers
Dimensions
Length, Main Rotor Blade to Tail Rotor 9.40 m
Length, Nose to Tail 7.28 m
Rotor Diameter 8.1 m
Height 2.66 m
Width, Skid to Skid 1.90 m
Width, Fuselage 1.40 m
Width, Tail 1.70 m
Automotive
Engine Name 1 x Rolls-Royce 250-C20R
Engine Type INA
Engine Power 450 hp
Maximum Range, at Sea Level 478 km
Maximum Range, at 5,000 feet 537 km
Fuel Capacity 242 liters
Speed, Never-Exceed 282 km/h
Speed, Cruise (At Sea Level) 249 km/h
Speed, Cruise (At 5,000 feet) 246 km/h
Speed, Economical 222 km/h
Climb Rate 540 m/min
Ceiling 4,230 m
Maximum Operating Altitude 4,877 m
Hover, In Ground Effect 2,590 m
Hover, Outof Ground Effect 1,830 m
Endurance 2.8 hours
Internal Fuel Tanks 240 liters
Optional Aux Tank 80 liters
Communications
Radio Rockwell Collins VHF-251/231 navigation receiver
Transmitter/Receiver Honeywell KY196 transmitter/receiver and KT76 transponder or a Rockwell Collins VHF-251 and TDR-950 transceiver and responder
Wing Mounted Weapons
Note There is a variety of different types of Armament that can be equipped on the MD 500. Examples include the following: Armament * four TOW anti-tank missiles, or * two 7.62mm General Electric M134 Miniguns plus ammunition, or * four General Dynamics Stinger air-to-air missile, or * Mk 44 or Mk 46 lightweight torpedoes (ASW Version), or * two seven-shot rocket pods * .50-cal machine-gun pods, or * 7- or 12-tube 2.75-in rocket pods, or * 40-mm grenade launcher
MiniGun
Name M134 Minigun
Type 7.62×51mm NATO six-barrel rotary machine gun
Combat Load 2 X M134 Miniguns
Manufacturer General Electric, Dillon Aero, Garwood Industries, Profense
In Service 1962-Present
Proliferation Widely Proliferated
Length 801.6 mm
Barrel Length 558.8 mm
Weight 39 kg
Barrels 6 ea
Action Electrically driven rotary breech
Rate of Fire 2,000–6,000 rpm
Maximum Firing Range 1,000 m
Feed System Disintegrating M13 linked belt or linkless feed; dependent on installation [500-5,000-round belt]
Sights Dependent on installation; no fixed sights
Ammunition
Type Rifle
Caliber 7.62 mm
Cartridge 7.62×51mm NATO
Muzzle Velocity 853 m/s
Basic Load INA
Fire Control
Fire Control System Type INA
Fire Control Radar INA
Digital or Analog Cockpit Analog
Direction Finder Honeywell KR-85 automatic direction finder
Laser Designator INA
Navigation System Honeywell dual KX175 navigation system
Night-Flying Capable Yes, night-flying lighting
Position Location System Yes
Gyroscope Attitude and directional gyroscopes
Rate-Climb Indicator. Yes
Protection
Armor Type INA
Crew Cabin The crew cabin features a glazed nose for maximum forward visibility.
Stealth Properties No
Heat Signature Reduction INA
Add on Armor INA
NBC Protection Yes
EW INA
EW Counter Measures/CCM INA
Counter Measures (Chaff/Flares) INA
Details
Country of Origin United States
Category Rotary Wing Aircraft
Air > Rotary Wing Aircraft
Filter Label
M
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
Width
Height
2.66 m
Weight
Operators (17)
United States
Italy
Japan
South Korea
North Korea
Afghanistan
Argentina
Chile
Colombia
El Salvador
Finland
Kenya
Lebanon
Malaysia
Mexico
Panama
Philippines
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