M61 Vulcan

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M61 Vulcan
An unmounted M61 Vulcan.
TypeSix-barreled Gatling-style rotary cannon
Place of originUnited States
Service history
In service1959–present
Used byUnited States/NATO
WarsVietnam War, Gulf War, War on Terror
Production history
Designed1946
ManufacturerGeneral Electric
VariantsSee below
Specifications
Mass248 pounds (112 kg) (excluding feed system) (M61A1) or 202 pounds (92 kg) (excluding feed system) (M61A2)
(HEI) 100 g (3.5 oz) (projectile)
Length71.93 in (1,827 mm)
Cartridge20×102mm
Caliber20 mm (0.787 in)
Barrels6
ActionHydraulically operated, electrically fired, Gatling
Rate of fire6,000 rounds per minute (M61A1)
6,600 rounds per minute (M61A2)
Muzzle velocity3,450 feet per second (1,050 m/s) (with PGU-28/B round)
Feed systemBelt or linkless feed system

The M61 Vulcan is a hydraulically or pneumatically driven, six-barreled, air-cooled, electrically fired Gatling-style rotary cannon which fires 20 mm rounds at an extremely high rate. The M61 and its derivatives have been the principal cannon armament of United States military fixed-wing aircraft for fifty years. The M61 was originally produced by General Electric, and after several mergers and acquisitions is currently produced by General Dynamics.[1]

Development

At the end of World War II, the United States Army began to consider new directions for future military aircraft guns. The higher speeds of jet-engined fighter aircraft meant that achieving an effective number of hits would be extremely difficult without a much higher volume of fire. While captured German designs (principally the Mauser MG 213C) showed the potential of the single-barrel revolver cannon, the practical rate of fire of such a design was still limited by ammunition feed and barrel wear concerns. The Army wanted something better, combining extremely high rate of fire with exceptional reliability.

In response to this requirement, the Armament Division of General Electric resurrected an old idea: the multi-barrel Gatling gun. The original Gatling gun had fallen out of favor because of the need for an external power source to rotate the barrel assembly, but the new generation of turbojet-powered fighters offered sufficient electric power to operate the gun, and electric operation offered reliability superior to a gas operated weapon. With multiple barrels, the rate of fire per barrel could be lower than a single-barrel revolver cannon while still giving a superior total rate of fire. The idea of powering a Gatling gun from an external electric power source was not a novel idea at the end of the World War II era, as Richard Jordan Gatling himself did just that in a patent he filed in 1893.[2]

The Army issued General Electric the contract in 1946 for "Project Vulcan", a six-barrel weapon capable of firing 7,200 rounds per minute (rpm).[3] Although European designers were moving towards heavier 30 mm weapons for better hitting power, the U.S. initially concentrated on a powerful .60 caliber (15 mm) cartridge designed for a pre-war anti-tank rifle, expecting that the cartridge's high muzzle velocity would be beneficial for improving hit ratios on high speed targets. The first GE prototypes of the .60 caliber T45 were ground-fired in 1949; it achieved 2,500 rpm, which was increased to 4,000 rpm by 1950. By the early 1950s, the USAF decided that high velocity alone might not be sufficient to ensure target destruction and tested 20 mm and 27 mm alternatives based on the .60 caliber cartridge. These variants of the T45 were known as the T171 and T150 respectively, and were first tested in 1952. Eventually, the 20 x 102 mm cartridge was determined to have the desired balance of projectile and explosive weight and muzzle velocity.

The development of the Lockheed F-104 Starfighter revealed that the T171 Vulcan (later redesignated M61) suffered problems with its linked ammunition, being prone to misfeed and presenting a foreign object damage (FOD) hazard with discarded links. A linkless ammunition feed system was developed for the upgraded M61A1, which subsequently became the standard cannon armament of U.S. fighters.

In 1993, General Electric sold its aerospace division, including GE Armament Systems along with the design and production tooling for the M61 and GE's other rotary cannon, to Martin Marietta. After Martin's merger with Lockheed, the rotary cannon became the responsibility of Lockheed Martin Armament Systems. Lockheed Martin Armament Systems was later acquired by General Dynamics, who currently produce the M61 and its various offspring.[1]

Description

M61 Vulcan at the Miramar Airshow

The Vulcan is a Gatling gun: each of the cannon's six barrels fires once in turn during each revolution of the barrel cluster. The multiple barrels provide both a very high rate of fire—around 100 rounds per second—and contribute to long weapon life by minimizing barrel erosion and heat generation. Mean time between jams or failures is in excess of 10,000 rounds, making it an extremely reliable weapon. The success of the Vulcan Project and its subsequent progeny, the very-high-speed Gatling gun, has led to guns of the same configuration being referred to as Vulcan Cannon, which can sometimes confuse nomenclature on the subject.

Most aircraft versions of the M61 are hydraulically driven and electrically primed. The gun rotor, barrel assembly and ammunition feed system are rotated by a hydraulic drive motor through a system of flexible drive shafts. The round is fired by an electric priming system where an electrical current from a firing lead passes through the firing pin to the primer as each round is rotated into the firing position. The self-powered version, the GAU-4 (called M130 in Army service), is gas-operated, tapping gun gas from three of the six barrels to operate the mechanism. The self-powered Vulcan weighs about 10 pounds (4.5 kg) more than its electric counterpart, but requires no external power source to operate.

An M61 ammunition belt

The initial M61 used linked, belted ammunition, but the ejection of spent links created considerable (and ultimately insuperable) problems. The original weapon was soon replaced by the M61A1, with a linkless feed system. Depending on the application, the feed system can be either single-ended (ejecting spent cases and unfired rounds) or double-ended (returning casings back to the magazine). A disadvantage of the M61 is that the bulk of the weapon, its feed system, and ammunition drum makes it difficult to fit it into a densely packed airframe. The feed system must be custom-designed for each application, adding 300–400 lb (140–180 kg) to the complete weapon. Most aircraft installations are double-ended, because the ejection of empty cartridges can cause a foreign-object damage (FOD) hazard for jet engines and because the retention of spent cases assists in maintaining the center of gravity of the aircraft. The first aircraft to carry the M61A1 was the C model of the F-104, starting in 1959.

A lighter version of the Vulcan developed for use on the F-22 Raptor, the M61A2, is mechanically the same as the M61A1, but with thinner barrels to reduce overall weight to 202 pounds (92 kg). The rotor and housing have also been modified to remove any piece of metal not absolutely needed for operation and replaces some metal components with lighter weight materials. The F/A-18E/F also uses this version.[4]

The Vulcan's rate of fire is typically 6,000 rounds per minute, although some versions (such as that of the AMX and the F-106 Delta Dart) are limited to a lower rate, and others have a selectable rate of fire of either 4,000 or 6,000 rounds per minute. The M61A2's lighter barrels allow a somewhat higher rate of fire up to 6,600 rounds per minute.

Ammunition

M61 on display.

Practically no powered rotary cannon is supplied with enough ammunition for a full minute of firing, because of the weight of the ammunition. In order to avoid using the few hundred rounds carried in a matter of a single trigger pull, a burst controller is generally used to limit the number of rounds fired at each trigger pull. Bursts of from 2 or 3 up to 40 or 50 can be selected.

Until the late 1980s the M61 primarily used the M50 series of ammunition in various types, typically firing a 3.5 oz (100 gram) projectile at a muzzle velocity of about 3,380 feet per second (1,030 m/s). A variety of Armor-Piercing Incendiary (API), High Explosive Incendiary (HEI), and training rounds are available. Around 1988 a new round was introduced, the PGU-28/B,[5] which is now standard for US Navy and USAF aircraft. The PGU-28/B is a "low-drag" round designed to reduce in-flight drag and deceleration, and has a slightly increased muzzle velocity of 3,450 feet per second (1,050 m/s). It is a semi-armor piercing high explosive incendiary (SAPHEI) round, providing substantial improvements in range, accuracy, and power over the preceding M56A3 HEI round. The PGU-28/B has not been without problems, however. A 2000 USAF safety report noted 24 premature detonation mishaps (causing serious damage in many cases) in 12 years with the SAPHEI round, compared to only two such mishaps in the entire recorded history of the M56 round. The report estimated that the current PGU-28/B had a potential failure rate 80 times higher than USAF standards permit.[6]

The main types of combat rounds and their main characteristics are listed in the table below.

Designation Type Projectile Weight [g] Bursting charge [g] Muzzle Velocity [m/s] Description
M53 API ? 4.2 g incendiary[7] 1030 6.3 mm RHA penetration at 0 degree impact angle and 1000 m range.[7]
M56A3/A4 HEI 102[8] 9 g HE (RDX/wax/Al) and 1.5 g incendiary[7][8] 1030 Nose fuzed round, no tracer. 2 m effective radius to produce casualties to exposed personnel.[7] Fragmentation hazard out to 20 m.[8] 12.5 mm RHA penetration at 0 degree obliquity at 100m range.[7]
PGU-28A/B SAPHEI 102.4 [9] 10 g[8] 1050 Multi-purpose fuzeless round with an incendiary charge in the nose setting off the HE behind it with a slight delay to maximize lethality against aircraft. No tracer or self-destruct. A zirconium pellet at the bottom of the HE cavity provides additional incendiary effect.

Applications

West German Air Force F-104
Door opening to the F-22's internally mounted gun.

The Vulcan was first used in the F-104 Starfighter. The gun was also used in the F-105 Thunderchief in combat against Soviet-designed MiG fighters over Vietnam. It was installed in the Air Force's A-7D version of the A-7 Corsair II where it replaced the Naval versions' standard dual cannon, and subsequently adopted by the Navy on the A-7E[10] and in future fighters. Significantly it was designed into the F-4E Phantom II; no previous F-4 had a cannon as it had been believed that missiles had made guns obsolete. Combat experience in Vietnam showed that a gun could be more effective than guided missiles in many combat situations, and that an externally carried gun pod was less effective than an internal gun.

The Vulcan was later fitted into the weapons bay of some F-106 Delta Dart models and the F-111 Aardvark. It was also adopted as standard in the teen-series air superiority fighters, the F-14 Tomcat, the F-15 Eagle, F-16 Fighting Falcon and F/A-18 Hornet. Other aircraft include the Italian/Brazilian AMX International AMX (on Italian aircraft only), and the F-22 Raptor. It was fitted in a side-firing installation on the AC-119, some marks of the AC-130 gunships, and was used in the tail turrets of both the Convair B-58 Hustler and Boeing B-52H Stratofortress bombers. Japan's Mitsubishi F-1 carried one internally mounted JM61A1 Vulcan with 750 rounds.[10]

Two gun pod versions, the SUU-16/A (also designated M12 by the US Army) and improved SUU-23/A (US Army M25), were developed in the 1960s, often used on gunless versions of the F-4. The SUU-16/A uses the electric M61A1 with a ram-air turbine to power the motor. This proved to cause serious aerodynamic drag at higher speeds, while speeds under 400 miles per hour (640 km/h) did not provide enough air flow for maximum rate of fire. The subsequent SUU-23/A uses the GAU-4/A self-powered Vulcan, with an electric inertia starter to bring it up to speed. Both pods ejected empty cases and unfired rounds rather than retaining them. Both pods contained 1,200 rounds of ammunition, with a loaded weight of 1,615 pounds (733 kg) and 1,720 pounds (780 kg) respectively. During service in the Vietnam War the pods proved to be relatively inaccurate: the pylon mounting was not rigid enough to prevent deflection when firing, and repeated use would misalign the pod on its pylon, making matters worse.

A variant with much shorter barrels, designated the M195 was also developed for use on the M35 Armament Subsystem for use on the AH-1G Cobra helicopter. This variant fed from ammunition boxes fitted to the landing skid and was developed to provide the AH-1 helicopter with a longer-range suppressive fire system before the adoption of the M97 Universal Turret mounting the M197 cannon.

The M61 is also the basis of the US Navy Mk 15 Phalanx CIWS system and the M163 VADS Vulcan Air Defense System (the M168 variant is used).

See also

References

  1. ^ a b "M61 20mm cannon". Federation of American Scientists. April 23, 2000. Retrieved 2009-02-28.
  2. ^ http://img294.imageshack.us/img294/2433/eleckeygatling.jpg
  3. ^ "The Gatling Gun". Retrieved 2008-09-28. {{cite web}}: |archive-url= is malformed: timestamp (help)
  4. ^ F/A-18E/F Super Hornet Maritime Strike Attack Aircraft "..features new lightweight gun system is the General Dynamics M61A2, which has a switchable firing rate of 4,000 or 6,000 shots per minute and a fully integrated linkless ammunition feed system"
  5. ^ "PGU-27A/B TP/PGU-28A/B SAPHEI/ GU-30A/B TP-T". GlobalSecurity.org. Retrieved 2008-09-28.
  6. ^ [1] [dead link]
  7. ^ a b c d e "20-Millimeter at aircav.com, http://www.aircav.com/cobra/ammo20.html
  8. ^ a b c d ORDATA: Ordnance Identification Tool, http://maic.jmu.edu/ordata
  9. ^ "PGU-27A/B TP/PGU-28A/B SAPHEI/PGU-30A/B TP-T". GlobalSecurity.org. Retrieved 2010-01-25.
  10. ^ a b Chant, Christopher (1987). A Compendium of Armaments and Military Hardware. Routledge. pp. 65–70, 106, 114–115, 341–343, 363, 389, 404–405. ISBN 978-0-7102-0720-3.

External links

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