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Deadliest Gun Ever Invented – Million

Rounds Per Minute – Metal Storm

Wise Wanderer

Published on Aug 5, 2014

www.metalstormusa.com/
Metal Storm Limited is a research and development company that specialises in electronically initiated stacked projectile weapons technology. Metal Storm is both the name of the company and the technology.The company is based in Brisbane, Australia with a subsidiary in Washington DC, U.S.A. Metal Storm owns the proprietary rights to the electronic ballistics technology invented by J. Mike O’Dwyer.
Metal Storm has created a 36-barreled stacked projectile machine gun, boasting the highest rate of fire in the world. The prototype weapon demonstrated a firing rate of slightly over one million rounds per minute for a 180-round burst.
Metal storm is one of the most devastating / deadliest weapons ever invented. This amazing weapon combines the magazine with the barrel, cutting moving parts down to zero. With the bullets simply lined up next to each other in the barrel, this gun can fire at absolutely staggering rates. There’s no hammer pulling the trigger sends a series of electrical signals down the barrel to the bullet. This weapon can intercept supersonic weapons it’s reliable. It’s also the most powerful automatic weapon ever made. – The Discovery Channel put together a great piece showing just how this amazing weapons operates.
With the ability to fire 16,000 rounds of ammunition each second, the Metal Storm Stacked Projectile is one of the most fearsome military weapons in development.

Music: “Here Today Gone Tomorrow” by Dhruva Aliman
and “Warfish” by Dhruva Aliman
https://dhruvaaliman.bandcamp.com/alb…
http://www.dhruvaaliman.com

 

UNFORTUNATELY …………….

BRISBANE weapons maker Metal Storm – which pitched ideas ranging from an electronic handgun to a three-shot grenade launcher – has finally run out of cash after 18 years of development.

Voluntary administrators were called in this morning to Metal Storm, which has chalked up $115 million in losses.

Metal Storm was forced into receivership in 2012.

It was a fierce system while it lasted and may show up again sometime in the future.

 

 

DEADLY FAST us military M134D

gatling machine gun

ArmedForcesUpdate

 
 

Published on Dec 27, 2014

Another great video on US military Gatling machine guns The Dillon M134D Gatling Gun is the finest small caliber, defense suppression weapon available. It is a six barreled, electrically driven machine gun chambered in 7.62mm NATO and fires at a fixed rate of 3,000 shots per minute. Gatling Guns typically feed from a 3,000 or 4,000 round magazine. They are capable of long periods of continuous fire without threat or damage to the weapon making them an excellent choice for defensive suppression.

Dillon Guns are reliable. The M134D has system life in excess of one million rounds and an average time between stoppage of 30,000 rounds. In the unlikely event of a stoppage the weapon can be serviced and made operational again in under a minute. The multi barrel design means that each barrel only experiences a 500 round per minute rate of fire. This allows for repeated long bursts of fire and a barrel group life of 200,000 rounds.

Dillon Gatling Guns are in service with the US and Allied Armed Forces. The standard application is as helicopter crew served and fixed forward fire installations. In addition to their more traditional roles, Dillon Gatlings are supplanting M2 50 cal. Heavy Machine Guns and M240′s on a number of the US Army’s vehicles. Dillon M134s are also in service with the US and British navies in the fleet protection role and Special Operations fire support role.

Dillon M134 Gatling Guns are entirely new production weapons. Dillon guns are sold as complete weapon systems or as component upgrade packages for older GE M134 systems.

Minigun

From Wikipedia, the free encyclopedia
“M134″ redirects here. For the highway, see M-134 (Michigan highway).
Machine Gun, High Rate, 7.62mm, M134

Dillon Aero’s M134D-H (H for Hybrid) combines the titanium and skeletonized parts that were engineered for use in the M134D-T minigun with the steel housing of the previous M134D.
Type Rotary machine gun
Place of origin United States
Service history
In service 1963–present
Used by See Users below
Wars War in Afghanistan[1][2]
Production history
Designer General Electric
Designed 1960
Manufacturer General Electric, Dillon Aero, Garwood Industries, Profense
Produced 1962–present
Variants See Design and variants below
Specifications
Weight 85 lb (39 kg) (41 lb (19 kg) lightweight mod.)
Length 801.6 mm (31.56 in)
Barrel length 558.8 mm (22.00 in)

Cartridge 7.62×51mm NATO
Caliber 7.62 mm (0.308 in)
Barrels 6
Action Electrically driven rotary breech
Rate of fire Variable, 2,000–6,000 rpm
Muzzle velocity 2,800 ft/s (853 m/s)
Maximum firing range 3,280 ft (1,000 m, 1,093 yd)
Feed system Cartridge on disintegrating link belt or linkless feed; dependent on installation [500-5,000-round belt]
Sights Dependent on installation; no fixed sights

The M134 Minigun is a 7.62×51mm NATO, six-barrel rotary machine gun with a high rate of fire (2,000 to 6,000 rounds per minute) which can also fire at a high sustained rate.[3] It features Gatling-style rotating barrels with an external power source, normally an electric motor. The “Mini” in the name is in comparison to larger caliber designs that use a rotary barrel design, such as General Electric’s earlier 20-millimeter M61 Vulcan, and “gun” for the use of rifle caliber bullets instead of shells used by an autocannon.

The Minigun is used by several branches of the U.S. military. Versions are designated M134 and XM196 by the United States Army, and GAU-2/A and GAU-17/A by the U.S. Air Force and U.S. Navy.

“Minigun” refers to a specific model of weapon that General Electric originally produced, but the term “minigun” has popularly come to refer to any externally powered rotary-style gun of rifle caliber. The term is sometimes used loosely to refer to guns of similar rates of fire and configuration regardless of power source and caliber.

Contents

History

Background: electrically driven Gatling gun

The ancestor to the modern minigun was a hand cranked mechanical device invented in the 1860s by Richard Jordan Gatling. Gatling later replaced the hand-cranked mechanism of a rifle-caliber Gatling gun with an electric motor, a relatively new invention at the time. Even after Gatling slowed down the mechanism, the new electric-powered Gatling gun had a theoretical rate of fire of 3,000 rounds per minute, roughly three times the rate of a typical modern, single-barreled machine gun. Gatling’s electric-powered design received U.S. Patent #502,185 on July 25, 1893.[4] Despite Gatling’s improvements, the Gatling gun fell into disuse after cheaper, lighter-weight, recoil and gas operated machine guns were invented; Gatling himself went bankrupt for a period.[5]

During World War I, several German companies were working on externally powered guns for use in aircraft. Of those, the best-known today is perhaps the Fokker-Leimberger, an externally powered 12-barrel rotary gun using the 7.92×57mm Mauser round; it was claimed to be capable of firing over 7,000 rpm, but suffered from frequent cartridge-case ruptures[6] due to its “nutcracker”, rotary split-breech design, which is fairly different from that of a Gatling.[7] None of these German guns went into production during the war, although a competing Siemens prototype (possibly using a different action) which was tried on the Western Front scored a victory in aerial combat.[6] The British also experimented with this type of split-breech during the 1950s, but they were also unsuccessful.[8]

Minigun: 1960s–Vietnam

In the 1960s, the United States Armed Forces began exploring modern variants of the electric-powered, rotating barrel Gatling-style weapons for use in the Vietnam War. American forces in the Vietnam War, which used helicopters as one of the primary means of transporting soldiers and equipment through the dense jungle, found that the thin-skinned helicopters were very vulnerable to small arms fire and rocket-propelled grenade (RPG) attacks when they slowed down to land. Although helicopters had mounted single-barrel machine guns, using them to repel attackers hidden in the dense jungle foliage often led to barrels overheating or cartridge jams.[citation needed]

 
A U.S. Air Force rotary-wing crewman fires a minigun during the Vietnam War.

In order to develop a weapon with a more reliable, higher rate of fire, General Electric designers scaled down the rotating-barrel 20 mm M61 Vulcan cannon for 7.62×51mm NATO ammunition. The resulting weapon, designated M134 and known popularly as the Minigun, could fire up to 4,000 rounds per minute without overheating. The gun was originally specified to fire at 6,000 rpm, but this was later lowered to 4,000 rpm.

The Minigun was mounted on Hughes OH-6 Cayuse and Bell OH-58 Kiowa side pods; in the turret and on pylon pods of Bell AH-1 Cobra attack helicopters; and on door, pylon and pod mounts on Bell UH-1 Iroquois transport helicopters.[citation needed] Several larger aircraft were outfitted with miniguns specifically for close air support: the Cessna A-37 Dragonfly with an internal gun and with pods on wing hardpoints; and the Douglas A-1 Skyraider, also with pods on wing hardpoints. Other famous gunship airplanes were the Douglas AC-47 Spooky, the Fairchild AC-119, and the Lockheed AC-130.[citation needed]

Dillon Aero minigun

The U.S. government had procured some 10,000 miniguns during the Vietnam War. By 1975, production of spare parts had ceased with the Army in possession of a large inventory. By 1985, there were few spares left in the inventory. Units that received miniguns could not maintain them, so by the 1990s only Task Force 160 (later named the 160th Special Operations Aviation Regiment (Airborne) or 160th SOAR) and some Navy Special Boat Units kept them in regular use. Around 1995, the 160th SOAR began acquiring spare miniguns. Industry had a difficult time reproducing parts according to the original blueprints, so models that were being procured were mechanically unreliable and mixed with the inventory of working spares. This resulted in using a mixed batch of working and unreliable weapons. This fact was unknown to the 160th SOAR, and the use of miniguns that would not work shook the unit’s confidence in the system. The 160th was on the verge of dropping the Minigun from its inventory entirely, which would essentially have ended its service life in the U.S. military.[9]

Around 1990, Dillon Aero acquired a large number of miniguns and spares from “a foreign user”. The guns kept failing to shoot continuously, revealing that they were actually worn-out weapons. The company decided to fix the problems encountered, rather than simply putting the guns into storage. Fixing failure problems ended up improving the minigun’s overall design.[9] Dillon’s efforts to improve the minigun reached the 160th SOAR, and Dillon was invited to Fort Campbell, Kentucky to demonstrate its products. A delinker–used to separate cartridges from ammunition belts and feed them into the gun housing–; and other parts were tested on Campbell’s ranges. The 160th SOAR liked the delinker’s performance and began ordering them by 1997. This prompted Dillon to improve other design aspects, including the bolt, housing and barrel. Between 1997 and 2001, Dillon Aero was producing 25–30 products a year. In 2001, it was working on a new bolt design that increased performance and service life. By 2002 virtually every component of the minigun had been improved, so Dillon began producing complete weapons with improved components. The guns were purchased quickly by the 160th SOAR as its standardized weapon system. The gun then went through the Army’s formal procurement system approval process and in 2003 the Dillon Aero minigun was certified and designated M134D.[9]

The core of the M134D was a steel housing and steel rotor. To focus on weight reduction, a titanium housing and rotor were introduced, creating the M134D-T. This reduced weight from 62 pounds (28 kg) to 41 pounds (19 kg). The gun housing had a 500,000 round lifespan before it wore out, which was higher than a conventional machine gun’s 40,000 round lifespan but was a reduced time for a rotary gun. A hybrid of the two weapons resulted in the M134D-H, which had a steel housing and titanium rotor. It was cheaper with the steel component, was only one pound (450 grams) heavier than the M134D-T, and had an increased lifespan of 1 million rounds.[10] The M134D-H is currently in use on various 160th Regiment platforms.[9]

Dillon also created specialized mounts and ammunition-handling systems. Initially, mounts were only made for aviation systems. Then from 2003 to 2005, the Navy began mounting Dillon miniguns on specialized small boats. In 2005, the Naval Surface Warfare Center Crane Division procured guns to mount on Humvees. In Iraq, US Army Special Forces units on the ground were frequently engaged by opposition forces, so they mounted M134D miniguns on their vehicles for additional firepower. After several engagements the attackers seemed to avoid vehicles with miniguns. Later the Special Forces units began concealing their weapons so opposition troops would not know which weapon they were facing.[9]

Garwood Industries minigun

Garwood Industries created the M134G version with several modifications to the original GE system. The optimum rate of fire was determined by Garwood to be around 3,200 rounds per minute (rpm). The M134G is being produced with this firing rate as well as 4,000 rpm and the previous standard 3,000 rpm rate.[11]

Garwood Industries made several other modifications to the 1960s Minigun design in order to meet modern day military and ISO standards.[11] This includes modifications to the drive motor, feeder and barrel clutch assembly.[12]

Design and variants

 
A Royal Navy minigun, separated from mounting and ammunition

The basic minigun is a six-barrel, air-cooled, and electrically driven rotary machine gun. The electric drive rotates the weapon within its housing, with a rotating firing pin assembly and rotary chamber.[13] The minigun’s multi-barrel design helps prevent overheating, but also serves other functions. Multiple barrels allow for a greater capacity for a high firing rate, since the serial process of firing/extraction/loading is taking place in all barrels simultaneously. Thus, as one barrel fires, two others are in different stages of shell extraction and another three are being loaded. The minigun is composed of multiple closed-bolt rifle barrels arranged in a circular housing. The barrels are rotated by an external power source, usually electric, pneumatic, or hydraulic. Other rotating-barrel cannons are powered by the gas pressure or recoil energy of fired cartridges. A gas-operated variant, designated XM133, was also developed.[14] It is near identical but has barrels with ports that align with the piston drive in the center of the barrel cluster. It fired over 3000 rpm but was not put into production.[citation needed]

While the weapon can feed from linked ammunition, it requires a delinking feeder to strip the links as the rounds are introduced to the chambers. The original feeder unit was designated MAU-56/A, but has since been replaced by an improved MAU-201/A unit.[15]

 
A U.S. Navy Special Warfare Combatant-craft Crewmen (SWCC) firing a Minigun at the Stennis Space Center in Mississippi, August 2009

The General Electric minigun is in use in several branches of the U.S. military, under a number of designations. The basic fixed armament version was given the designation M134 by the United States Army, while the same weapon was designated GAU-2/A (on a fixed mount) and GAU-17/A (flexible mount) by the United States Air Force (USAF) and United States Navy (USN). The USAF minigun variant has three versions, while the US Army weapon appears to have incorporated several improvements without a change in designation. The M134D is an improved version of the M134 designed and manufactured by Dillon Aero,[16] while Garwood Industries manufactures the M134G variant.[17] Available sources show a relation between both M134 and GAU-2/A and M134 and GAU-2B/A.[18][19] A separate variant, designated XM196, with an added ejection sprocket was developed specifically for the XM53 Armament Subsystem on the Lockheed AH-56 Cheyenne helicopter.[20]

Another variant was developed by the USAF specifically for flexible installations, beginning primarily with the Bell UH-1N Twin Huey helicopter, as the GAU-17/A. Produced by General Dynamics, this version has a slotted flash hider. The primary end users of the GAU-17/A have been the USN and the United States Marine Corps (USMC), which mount the gun as defensive armament on a number of helicopters and surface ships. GAU-17/As from helicopters were rushed into service for ships on pintle mountings taken from Mk16 20 mm guns for anti-swarm protection in the Gulf ahead of the 2003 Iraq War – 59 systems were installed in 30 days.[21] The GAU-17/A is designated Mk 44 in the machine gun series[21] and is generally known as the Mk 44 when installed on British warships.

The weapon is part of both the A/A49E-11 armament system on the UH-1N; and of the A/A49E-13 armament subsystem on the USAF Sikorsky HH-60H Pave Hawk helicopter. The weapons on these systems feature a selectable fire rate of either 2,000 or 4,000 rpm. There is mention of a possible GAUSE-17 designation (GAU-Shipboard Equipment-17), in reference to the system when mounted on surface ships, though this would not follow the official ASETDS designation system’s format.[22][23]

 
FAST Marine firing a GAUSE-17/A minigun

 
GAU-17/A
US Army designation US Air Force designation US Navy designation Description
XM134/M134 GAU-2/A N/A 7.62×51mm NATO GE “Minigun” 6-barreled machine gun
N/A GAU-2A/A N/A GAU-2/A variant; unknown differences
M134 GAU-2B/A Mk 25 Mod 0 GAU-2A/A variant; unknown differences
N/A GAU-17/A N/A GAU-2B/A variant; optimized for flexible use, uses either an MAU-201/A or MAU-56/A delinking feeder.
XM214 Microgun N/A N/A Scaled-down variant of the XM134 firing the 5.56×45mm NATO round.
XM196 N/A N/A M134/GAU-2B/A variant; housing modified by addition of an ejection sprocket; for use in the XM53 armament subsystem on the AH-56 helicopter

Gun pods and other aircraft mounts

 
SUU-11/A pod in the cargo door of an AC-47

One of the first applications of the weapon was in aircraft armament pods. These gun pods were used by a wide variety of fixed and rotary wing aircraft mainly during the Vietnam War, remaining in inventory for a period afterward. The standard pod, designated SUU-11/A by the Air Force and M18 by the U.S. Army, was a relatively simple unit, completely self-contained, with a 1,500-round magazine directly feeding delinked ammunition into the weapon. This means the Minigun fitted to the pod does not require the standard MAU-56/A delinking feeder unit.[24] A number of variations of this pod exist.

Initially on fixed-wing gunships such as the Douglas AC-47 Spooky and Fairchild AC-119, the side-firing armament was fitted by combining SUU-11/A aircraft pods, often with their aerodynamic front fairings removed, with a locally fabricated mount. These pods were essentially unmodified, required no external power, and were linked to the aircraft’s fire controls. The need for those pods for other missions led to the development and fielding of a purpose built “Minigun module” for gunship use, designated the MXU-470/A. These units first arrived in January 1967 with features such as an improved 2,000-round drum and electric feeder allowing simplified reloading in flight. The initial units were unreliable and were withdrawn almost immediately.[25] By the end of the year, however, the difficulties had been worked out and the units were again being fitted to AC-47s, AC-119s, AC-130s, and even being proposed for lighter aircraft such as the Cessna O-2 Skymaster.[26] A fit of two MXU-470/As was also tested on the Fairchild AU-23A Peacemaker, though the Royal Thai Air Force later elected to use another configuration with the M197 20 mm cannon.[27]

In September 2013, Dillon Aero released the DGP2300 gun pod for the M134D-H. It contains 3,000 rounds, enough ammunition to fire the minigun for a full minute. The system is entirely self-contained, so it can be mounted on any aircraft that can handle the weight, rotational torque, and recoil force (190 lb (86 kg)) of the gun. The pod has its own battery which can be wired into the aircraft’s electrical system to maintain a charge.[28]

 
MXU-470/A modules in an AC-47

 
Douglas AC-47 Spooky with SUU-11/A pods at Nha Trang Air Base in South Vietnam
US Army designation US Air Force designation Description
XM18 SUU-11/A Gun pod fitted with the GAU-2/A/M134 7.62 mm machine gun and fixed rate of fire of 4,000 RPM[29]
XM18E1/M18 SUU-11A/A SUU-11/A/XM18 variant; various improvements including additional auxiliary power and selectable fire-rate capability (2,000 or 4,000 RPM)[30]
M18E1/A1 SUU-11B/A SUU-11A/A/M18 variant; differences modified selectable fire-rate capability (3,000 or 6,000 RPM)[18]
N/A MXU-470/A Emerson Electric module for mounting a GAU-2B/A minigun; used in AC-47, AC-119G/K, and AC-130A/E/H aircraft

Various iterations of the minigun have also been used in a number of armament subsystems for helicopters, with most of these subsystems being created by the United States. The first systems utilized the weapon in a forward firing role for a variety of helicopters, some of the most prominent examples being the M21 armament subsystem for the UH-1 and the M27 for the OH-6. It also formed the primary turret-mounted armament for a number of members of the Bell AH-1 Cobra family. The weapon was also used as a pintle-mounted door gun on a wide variety of transport helicopters, a role it continues to serve in today.

US Navy designation Description
Mk 77 Mod 0 Machine gun mount for the GAU-2/Mk 25 Mod 0/GAU-17 series of machine guns; deck mount applications

References

Notes

  1.  
  1. Hogg, Ian (1989). Jane’s Infantry Weapons 1989–90 (15th ed.). Jane’s Information Group. p. 351. ISBN 0-7106-0889-6.

Sources

  • Ballad, Jack S. Development and Employment of Fixed-Wing Gunships, 1962–1972. Washington, DC: Office of Air Force History, United States Air Force, 1982.
  • Davis, Larry. Gunships: A Pictorial History of Spooky. TX: Squadron/Signal Publications, Inc, 1982. ISBN 0-89747-123-7
  • Gervasi, Tom. Arsenal of Democracy III: America’s War Machine, the Pursuit of Global Dominance. New York, NY: Grove Press, Inc, 1984. ISBN 0-394-54102-2.
  • Gunston, Bill. The Illustrated Encyclopedia of Aircraft Armament. New York, NY: Orion Books, 1988. ISBN 0-517-56607-9.
  • Jane’s Weapon Systems, 1986–1987. Ronald T Pretty, Ed. London, UK: Jane’s Publishing Company, Ltd, 1986. ISBN 0-7106-0832-2
  • United States. Headquarters, Department of the Army. FM 1–40 Attack Helicopter Gunnery. Washington, DC: Headquarters, Department of the Army, 1969.

External links

Categories:

TERRORIST KILLER us military GAU

19B 50 Cal Gatling Gun

ArmedForcesUpdate

 


 

GAU-19

From Wikipedia, the free encyclopedia
GAU-19/A
Type Heavy machine gun
Place of origin United States
Service history
Used by See History
Production history
Designer General Electric
Manufacturer General Dynamics
Produced 1983–present
Variants 3-barrel or 6-barrel
Specifications
Weight With feeder and transfer unit:139 lbs. (63 kg)
Length 53.9 in. (1,369 mm)
Barrel length 36 in. (914 mm)
Width 13.5 in. (343 mm)
Height 15 in. (381 mm)

Cartridge .50 BMG (12.7×99mm NATO)
Barrels 3
Action Electric
Rate of fire 1,000 or 2,000 rounds per minute
Muzzle velocity 2,910 fps (887 m/s)
Effective firing range 1,800 m
Maximum firing range 6,000 m
Feed system linkless or M9 linked belt

The GAU-19/A (GECAL 50), is an electrically driven Gatling gun that fires the .50 BMG (12.7×99mm) cartridge.

Contents

Technical specifications

The GAU-19/A is designed for a linkless feed, but can be fed from a standard M9 linked belt if a delinker feeder is used. The rate of fire is selectable to be either 1,000 or 2,000 rounds per minute. The Humvee armament kit version fires at 1,300 rounds per minute. The average recoil force when firing is 2.2kN. In January 2012, General Dynamics announced they would be delivering a new version designated GAU-19/B. It provides the same firepower in a lighter platform, weighing 48 kg.[1]

History

 
GAU-19/B mounted. Eurosatory Paris, 2016.

The GECAL 50 was first manufactured by General Electric, then by Lockheed Martin, and now by General Dynamics. Design work began in 1982. Early prototypes had six barrels, but a three-barreled configuration is now standard. The GAU-19/A was originally designed as a larger, more potent version of the M134 Minigun. Due to the loss of nine helicopters in Grenada, GE started building prototypes of the weapon in both a three-barreled and a six-barreled configuration. The six-barreled version was designed to fire 4,000 rounds per minute, and could be adapted to fire up to 8,000 rounds per minute. The GAU-19 takes 0.4 seconds to reach maximum firing rate.[2] Soon it was recommended as a potential armament for the V-22 Osprey.[3] The magazine would be located underneath the cabin floor and could be reloaded in-flight. However, plans to mount the gun were later dropped.[4] In 2005, the GAU-19/A was approved to be mounted on the OH-58D Kiowa helicopter. It also could have been used on the Army’s now cancelled ARH-70.[5] In January 2012, the U.S. Army ordered 24 GAU-19/B versions for use on helicopters. All were delivered by the next month.[1]

In 1999, the United States sent 28 GAU-19s to Colombia.[6]Oman is known to use the GAU-19/A mounted on their HMMWVs. The Mexican Navy uses MDH MD-902 series helicopters with the GAU-19/A system mounted for anti-narcotics operations.[7]

See also

Notes

  1.  

References

External links

Categories:

 

Most Powerful Grenade Launcher in

Action: Mk-19 During US Army

Training Session

Daily Military Defense & Archive

 

Mk 19 grenade launcher

From Wikipedia, the free encyclopedia
 

 
Mk 19 grenade launcher

A Mk 19 40 mm grenade launcher mounted on an M3 tripod
Type Automatic grenade launcher
Place of origin United States
Service history
In service 1968–present
Used by See Users
Wars
Production history
Designer Naval Ordnance Station Louisville
Designed 1966
Manufacturer Saco Defense Industries (now a division of General Dynamics Ordnance and Tactical Systems), Combined Service Forces, MKEK[4]
Unit cost $20,000[5]
Produced 1968–present
Variants Mk 19 Mod 0, Mk 19 Mod 1, Mk 19 Mod 2, Mk 19 Mod 3, Mk 19 Mod 4
Specifications
Weight 77.6 pounds (35.2 kg) (empty, without accessories)
Length 43.1 inches (1,090 mm)
Barrel length 16.25 inches (413 mm)
Width 9.46 inches (240.4 mm)
Height 7.8 inches (199 mm)

Cartridge 40×53 mm
Action Blowback (Advanced primer ignition)
Rate of fire 40 rpm (sustained)
60 rpm (rapid)
325–375 rpm (cyclic)
Muzzle velocity 790 feet per second (241 m/s) (average)
Effective firing range 1,500 m (1,600 yd)
Maximum firing range 2,212 m (2,419 yd)
Feed system 32- or 48-grenade belt

The Mk 19 grenade launcher (also known as the Mark 19) is an American 40 mm belt-fed automatic grenade launcher that was first developed during the Vietnam War. The first model (Mod 0) in 1966 was determined to be unreliable and unsafe, but a total of six Mod 1 launchers were successfully tested on U.S. Navy riverine patrol craft in the Mekong Delta in 1972. The Navy made further improvements to the weapon, resulting in the Mod 3 in 1976. The Mod 3 was adopted by the U.S Army in 1983 and remains in service to the present day.[6][7]

Contents

Overview

 
A U.S. Marine fires a Mk 19 40 mm grenade launcher in Quantico, Virginia in September 2000.

The Mk 19 is a belt-fed, blowback-operated, air-cooled, crew-served, fully automatic weapon that is designed not to cook off. It fires 40 mm grenades at a cyclic rate of 325 to 375 rounds per minute, giving a practical rate of fire of 60 rounds per minute (rapid) and 40 rounds per minute (sustained). The weapon operates on the blowback principle, which uses the chamber pressure from each fired round to load and re-cock the weapon. The Mk 19 can launch its grenade at a maximum distance of 2,212 meters (2,419 yd), though its effective range to a point target is about 1,500 meters (1,600 yd), since the large rear leaf sight is only graduated as far. The nearest safe distance to launch the grenade is 310 meters in training and 75 meters in combat. Though the Mk 19 has a flash suppressor, it serves only to save the eyesight of its operator, not concealing the weapon’s position. For night operation, a picatinny rail quadrant sight can be added for thermal and night vision optics.

The Mk 19A is a man-portable crew-served weapon that can fire from a tripod-mounted position or from a vehicle mount, with the latter being the preferred method, as the weapon alone weighs 77.6 pounds (35.2 kg). The primary ammunition for it is the high-explosive dual-purpose M430 grenade. On impact, the grenade can kill anyone within a radius of five meters, and wound them within a radius of 15 meters. It can also punch through 2 inches (5.1 cm) of rolled homogeneous armor with a direct hit (0-degree obliquity), which means it can penetrate most infantry fighting vehicles and armored personnel carriers. It is especially effective when used against enemy infantry formations. The ammunition comes in cans that hold a 32- or 48-grenade belt weighing 42 and 60 pounds (19 and 27 kg), respectively. Due to its low recoil and comparatively light weight, it has been adapted for use on many different platforms, including small attack boats, fast attack vehicles such as the Humvee (HMMWV), AAV and Stryker, military jeeps, and a large variety of naval mounts.

The Mk 19 automatic grenade launcher replaced the earlier Mk 18 hand-cranked multiple grenade launcher. The 40 mm ammunition used (40×53 mm) is not interchangeable with that used in the M203 (40×46 mm). The M203 ammunition develops a lower chamber pressure, and resultant lower muzzle velocity and range, compared to ammunition loaded for the Mk 19. The Mk 19 fires from an open bolt. The rounds are mechanically fed onto the bolt face with the pull of the charging handles. When the trigger is pressed, the bolt closes, and the firing pin is released. The recoil blows back the bolt, feeds a new round onto the bolt face, which pushes the expended casing off the bolt face.

Production of the Mk 19 is managed by Saco Defense Industries (now a division of General Dynamics Ordnance and Tactical Systems).

In November 2014, General Dynamics entered into an agreement with Advanced Material Engineering Pte Ltd, a subsidiary of Singapore Technologies Kinetics, to manufacture 40 mm high-velocity airburst ammunition for the U.S. military. The 40 mm airburst grenade uses a programmable, time-based fuse that computes and programs the detonation time into it, which counts down once fired to zero to detonate at the intended target point. The airburst ammunition is compatible with the Mk 19, which would give it greater effectiveness and lethality, particularly against concealed and defilade targets.[8]

The U.S. Army plans to introduce several new features to the Mk 19 in an upgrade package that could be introduced by late 2017. Initiatives include: increased muzzle velocity through a less resistant barrel; increased cyclic rate from an improved profile for the vertical cam to reduce the force needed to charge the weapon; enhancing reliability with a redesigned round-positioning block to decrease the chance of misfires; increased durability and shortened re-assembly time after maintenance from a new cocking cam and lever; and an updated mechanical sight utilizing up-to-date ammunition ballistic data to aid accuracy.[9]

 United States of America:[12] Currently in widespread use throughout the U.S. Armed Forces.
 

  • U.S. Navy sailors fire a Mk 19 40 mm grenade launcher during a training exercise in March 2003.

  • Mk 19 in use by Polish Land Forces

  • A Mexican Army Chevrolet Silverado equipped with a Mk 19 at a military checkpoint in March 2009

See also

References

  1.  
  1. “Sayfa bulunamadi”. anahaberyorum.com. Retrieved 5 November 2016.

External links

DEADLY KILLER us military GAU 8

Gatling Gun

ArmedForcesUpdate

 

 

GAU-8 Avenger

From Wikipedia, the free encyclopedia
GAU-8 Avenger

The GAU-8/A Avenger’s barrel and breech assembly
(ammunition drum off right edge of photo).
Type Gatling-type autocannon
Place of origin United States
Service history
In service 1977–present
Used by United States Air Force (Avenger)
Various navies (Goalkeeper)
Production history
Manufacturer General Electric
No. built Approx. 715[1]
Variants GAU-12/U Equalizer
GAU-13/A
Specifications
Weight 619.5 lb (281 kg)
Length 19 ft 10.5 in (6.06 m) (total system)
112.28 in (2.85 m) (gun only)
Barrel length 90.5 in (2.30 m)
Width 17.2 in (0.437 m) (barrels only)

Cartridge 30×173 mm
Caliber 30 mm caliber
Barrels 7-barrel (progressive RH parabolic twist, 14 grooves)
Action Electrically controlled, hydraulic-driven
Rate of fire 3,900 rpm (variable)
Muzzle velocity 3,324 ft/s (1,010 m/s) (API)
Effective firing range 4,000 feet (1,220 m)
Maximum firing range Over 12,000 feet (3,660 m)
Feed system Linkless feed system

The General Electric GAU-8/A Avenger is a 30 mm hydraulically driven seven-barrel Gatling-type autocannon that is typically mounted in the United States Air Force‘s Fairchild Republic A-10 Thunderbolt II. Designed specifically for the anti-tank role, the Avenger delivers very powerful rounds at a high rate of fire. The GAU-8/A is also used in the Goalkeeper CIWS ship weapon system, which provides defense against short-range threats such as highly maneuverable missiles, aircraft, and fast maneuvering surface vessels.

Contents

History

The GAU-8 was created as a parallel program with the A-X (or Attack Experimental) competition that produced the A-10. The specification for the cannon was laid out in 1970,[2] with General Electric and Philco-Ford offering competing designs. Both of the A-X prototypes, the YA-10 and the Northrop YA-9, were designed to incorporate the weapon, although it was not available during the initial competition; the M61 Vulcan was used as a temporary replacement. Once completed, the entire GAU-8 assembly (correctly referred to as the A/A 49E-6 Gun System)[3] represents about 16% of the A-10 aircraft’s unladen weight. Because the gun plays a significant role in maintaining the A-10′s balance and center of gravity, a jack must be installed beneath the tail of the plane whenever the gun is removed for inspection in order to prevent the aircraft from tipping rearwards.

 
GAU-8 closeup, showing the off-center mounting of the weapon and landing gear

The gun is placed slightly off center in the nose of the plane with the front landing gear positioned to the right of the center line, so that the actively firing cannon barrel is directly on the aircraft’s center line. The gun is loaded using Syn-Tech’s linked tube carrier GFU-8/E 30 mm Ammunition Loading Assembly cart. This vehicle is unique to the A-10 and the GAU-8.[4]

The A-10 and its GAU-8/A gun entered service in 1977. It was produced by General Electric, though General Dynamics Armament and Technical Products has been responsible for production and support since 1997 when the division was sold by Lockheed Martin to General Dynamics.[3]

Design

The GAU-8 itself weighs 620 pounds (280 kg), but the complete weapon, with feed system and drum, weighs 4,029 pounds (1,828 kg) with a maximum ammunition load. It measures 19 ft 5 12 in (5.931 m) from the muzzle to the rearmost point of the ammunition system, and the ammunition drum alone is 34.5 inches (88 cm) in diameter and 71.5 inches (1.82 m) long.[5] Power for operating the gun is provided by twin hydraulic motors pressurized from two independent hydraulic systems. The magazine can hold 1,174 rounds, although 1,150 is the typical load-out. Muzzle velocity when firing Armor-Piercing Incendiary rounds is 1,013 m/s, almost the same as the substantially lighter M61 Vulcan’s 20 mm round, giving the gun a muzzle energy of just over 200 kilojoules.[6]

The standard ammunition mixture for anti-armor use is a five-to-one mix of PGU-14/B Armor Piercing Incendiary, with a projectile weight of about 14.0 oz (395 grams or 6,096 grains) and PGU-13/B High Explosive Incendiary (HEI) rounds, with a projectile weight of about 13.3 oz (378 grams or 5,833 grains).[7] The PGU-14/B’s projectile incorporates a lightweight aluminum body, cast around a smaller caliber depleted uranium penetrating core.[8] The Avenger is lethal against tanks and all other armored vehicles.[9]

 
GAU-8 mounted in A-10

A very important innovation in the design of the GAU-8/A ammunition is the use of aluminum alloy cases in place of the traditional steel or brass.[10] This alone adds 30% to ammunition capacity for a given weight. The projectiles incorporate a plastic driving band to improve barrel life. The shells are imposing to examine and handle, measuring 11.4 inches (290 mm) in length and weighing 1.53 pounds (0.69 kg) or more.[5][10]

The Avenger’s rate of fire was originally selectable, 2,100 rounds per minute (rpm) in the low setting, or 4,200 rpm in the high setting.[11] Later this was changed to a fixed rate of 3,900 rpm.[12] In practice, the cannon is limited to one and two-second bursts to avoid overheating and conserve ammunition; barrel life is also a factor, since the USAF has specified a minimum life of at least 20,000 rounds for each set of barrels.[13] There is no technical limitation on the duration the gun may be continuously fired, and a pilot could potentially expend the entire ammunition load in a single burst with no damage or ill effects to the weapons system itself. However, this constant rate of fire would shorten the barrel life considerably and require added barrel inspections and result in shorter intervals between replacement.

 
30mm round next to a .30-06 Springfield for comparison

Each barrel is a very simple non-automatic design having its own breech and bolt. Like the original Gatling gun, the entire firing cycle is actuated by cams and powered by the rotation of the barrels.[10] The seven-barrel carriage assembly itself is driven by the aircraft’s dual hydraulic system.[13]

The GAU-8/A ammunition is linkless, reducing weight and avoiding a great deal of potential for jamming. The feed system is double-ended, allowing the spent casings to be recycled back into the ammunition drum,[14] instead of ejected from the aircraft, which would require considerable force to eliminate potential airframe damage. The feed system is based on that developed for later M61 installations, but uses more advanced design techniques and materials throughout, to save weight.[5]

Firing system

Accuracy

The GAU-8/A is extremely accurate and can fire 4,200 rounds per minute without complications. The 30-mm shell has twice the range, half the time to target, and three times the mass of projectiles fired by guns mounted in comparable close air support aircraft.[1]

 
The GAU-8/A Avenger Gatling gun next to a VW Type 1. Removing an installed GAU-8 from an A-10 requires first installing a jack under the aircraft’s tail to prevent it from tipping, as the cannon makes up most of the aircraft’s forward weight.

The muzzle velocity of the GAU-8/A is about the same as that of the M61 Vulcan cannon, but the GAU-8/A uses heavier ammunition and has superior ballistics. The time of flight of its projectile to 4,000 feet (1,200 m) is 30 percent less than that of an M61 round; the GAU-8/A projectile decelerates much less after leaving the barrel, and it drops a negligible amount, about 10 feet (3.0 m) over the distance. The GAU-8/A accuracy when installed in the A-10 is rated at “5 mil, 80 percent”, meaning that 80 percent of rounds fired will hit within a cone with an angle of five milliradians. According to Dennis R. Jenkins, author of Fairchild-Republic A/OA-10 Warthog, 5 milliradians equates to a 40 feet (12 meters) diameter circle at the weapon’s design range of 4,000 feet (1,200 m).[15] According to the milliradian system in use in the U.S. however, an angle of 1 milliradian equates to 1 meter (3.3 ft) diameter at 1,000 m (3,300 ft);[16][17] meaning 5 milliradians equates to 20 feet (6 m) circle at 4,000 feet (1,200 m). By comparison, the M61 has an 8-milliradian dispersion.[10][18]

Recoil

Because the gun’s recoil forces could push the entire plane off target during firing, the weapon itself is mounted laterally off-center, slightly to the portside of the fuselage centreline, with the actively “firing” barrel in the nine o’clock position (when viewed from the front of the aircraft), so that the firing barrel lies directly on the aircraft’s center line. The firing barrel also lies just below the aircraft’s center of gravity, being bore sighted along a line 2 degrees below the aircraft’s line of flight. This arrangement accurately centers the recoil forces, preventing changes in pitch or yaw when fired. This configuration also provides space for the front landing gear, which is mounted slightly off-center on the starboard side of the nose.[19]

The GAU-8/A utilizes recoil adapters. They are the interface between the gun housing and the gun mount. By absorbing (in compression) the recoil forces, they spread the time of the recoil impulse and counter recoil energy transmitted to the supporting structure when the gun is fired.

The A-10 engines were initially susceptible to flameout when subjected to gases generated in the firing of the gun. When the GAU-8 is being fired, the smoke from the gun can make the engines stop, and this did occur during initial flight testing.[2] Gun exhaust is essentially oxygen-free, and is certainly capable of causing flame-outs of gas turbines. The A-10 engines now have a self-sustaining combustion section. When the gun is fired the igniters come on to reduce the possibility of a flame-out.[20]

The average recoil force of the GAU-8/A is 10,000 pounds-force (45 kN),[3][21] which is slightly more than the output of one of the A-10′s two TF34 engines (9,065 lbf / 40.3 kN each).[22] While this recoil force is significant, in practice a cannon fire burst only slows the aircraft a few miles per hour in level flight.[20]

Variants

Some of the GAU-8/A technology has been transferred into the smaller 25 mm GAU-12/U Equalizer, which was developed for the AV-8B Harrier II aircraft. The GAU-12 is about the same size as the 20 mm M61. GE has also developed the GAU-13/A, a four-barreled weapon using GAU-8/A components, which has been tested in podded form as the GPU-5/A. The Avenger also forms the basis for the Dutch-developed Goalkeeper CIWS naval air-defence gun. No current or contemplated aircraft other than the A-10, however, carries the full-up Avenger system.[5]

Specifications

 
A side-view drawing of the GAU-8/A Avenger’s mounting location in the A-10′s forward fuselage
  • Precision: 80% of rounds fired at 4,000 feet (1,200 m) range hit within a 40 feet (12 m) diameter circle
  • Ammo:
  • Armor penetration of Armor-Piercing Incendiary ammunition, BHN-300 RHA, attack angle 30 degrees from vertical:[23]
    • 76mm at 300 meters
    • 69mm at 600 meters
    • 64mm at 800 meters
    • 59mm at 1,000 meters
    • 55mm at 1,220 meters

See also

General:

References

  1.  
  1. Berko Zecevic, Jasmin Terzic, Alan Catovic, Sabina Serdarevic-Kadic.“Dispersion of PGU-14 ammunition during air strikes by combat aircraft A-10 near urban areas”, page 800. University of Sarajevo, Mechanical Engineering Faculty, Sarajevo, Bosnia and Herzegovina. April 21 2010.
  • Spick, Michael. The Great Book of Modern Warplanes, Salamander Books, 2000. ISBN 1-84065-156-3.

External links

Wikimedia Commons has media related to GAU-8 Avenger.
Categories:

 

AC-130H Spectre Gunship • Airstrike

On Insurgents

Gung Ho Vids


 

Lockheed AC-130

From Wikipedia, the free encyclopedia
“AC-130″ redirects here. For the video game, see AC-130: Operation Devastation.
AC-130 Spectre/Spooky/Stinger II/Ghostrider
AC-130H Spectre gunship deploys flares in 2007
Role Ground-attack aircraft and close air support gunship
Manufacturer Lockheed
Lockheed Martin
Boeing
First flight AC-130A: 1966
Introduction AC-130A: 1968
AC-130H: 1969[1]
Retired AC-130A: 1995
AC-130H: 2015[1]
Status In service
Primary user United States Air Force
Number built 47 (in all variants)[citation needed]
Unit cost
AC-130H: US$132.4 million[citation needed]
AC-130U: US$253 million (2016)[citation needed]
Developed from Lockheed C-130 Hercules

The Lockheed AC-130 gunship is a heavily armed, long-endurance ground-attack variant of the C-130 Hercules transport fixed-wing aircraft. It carries a wide array of anti-ground oriented weapons that are integrated with sophisticated sensors, navigation, and fire-control systems. Unlike other military fixed-wing aircraft, the AC-130 relies on visual targeting. Because its large profile and low operating altitudes (around 7,000 ft) make it an easy target, it usually flies close air support missions at night.[2]

The airframe is manufactured by Lockheed Martin, while Boeing is responsible for the conversion into a gunship and for aircraft support.[3] Developed during the Vietnam War as ‘Project Gunship II’, the AC-130 replaced the Douglas AC-47 Spooky, or ‘Gunship I’. The sole operator is the United States Air Force, which uses the AC-130U Spooky and AC-130W Stinger II[4] variants for close air support, air interdiction, and force protection, with the AC-130J Ghostrider in development. Close air support roles include supporting ground troops, escorting convoys, and urban operations. Air interdiction missions are conducted against planned targets and targets of opportunity. Force protection missions include defending air bases and other facilities. AC-130Us are based at Hurlburt Field, Florida, while AC-130Ws are based at Cannon AFB, New Mexico; gunships can be deployed worldwide.[5] The squadrons are part of the Air Force Special Operations Command (AFSOC), a component of the United States Special Operations Command (SOCOM).[6]

The AC-130 has an unpressurized cabin, with the weaponry mounted to fire from the port side of the fuselage. During an attack, the gunship performs a pylon turn, flying in a large circle around the target, therefore being able to fire at it for far longer than in a conventional strafing attack. The AC-130H Spectre was armed with two 20 mm M61 Vulcan cannons, one Bofors 40 mm cannon, and one 105 mm M102 howitzer; after 1994, the 20 mm cannons were removed. The upgraded AC-130U Spooky has a single 25 mm GAU-12 Equalizer cannon in place of the Spectre’s two 20 mm cannons, an improved fire control system, and increased ammunition capacity. New AC-130Js based on the MC-130J Combat Shadow II special operations tanker were planned as of 2012. The AC-130W is armed with one 30 mm Bushmaster cannon, AGM-176 Griffin missiles, and GBU-39 Small Diameter Bombs (SDBs).[7]

Contents

Development

Origins

During the Vietnam War, the C-130 Hercules was selected to replace the Douglas AC-47 Spooky gunship (Project Gunship I) in order to improve mission endurance and increase capacity to carry munitions. Capable of flying faster than helicopters and at high altitudes with excellent loiter time, the use of the pylon turn allowed the AC-47 to deliver continuous accurate fire to a single point on the ground.[8][9]

 
AC-130H Spectre near Hurlburt Field, Florida in 1988

In 1967, JC-130A 54-1626 was selected for conversion into the prototype AC-130A gunship (Project Gunship II). The modifications were done at Wright-Patterson Air Force Base by the Aeronautical Systems Division. A direct view night vision telescope was installed in the forward door, an early forward looking infrared device in the forward part of the left wheel well, and Gatling guns fixed facing down and aft along the left side. The analog fire control computer prototype was handcrafted by RAF Wing Commander Tom Pinkerton at the USAF Avionics Laboratory at Wright-Patterson AFB. Flight testing of the prototype was performed primarily at Eglin Air Force Base, followed by further testing and modifications. By September 1967, the aircraft was certified ready for combat testing and was flown to Nha Trang Air Base, South Vietnam for a 90-day test program.[8] The AC-130 was later supplemented by the AC-119 Shadow (Project Gunship III), which later proved to be underpowered.

Seven more warplanes were converted to the “Plain Jane” configuration like the AC-130 prototype in 1968,[10] and one aircraft received the “Surprise Package” refit in 1969.[11] The Surprise Package upgrade included the latest 20 mm rotary autocannons and 40 mm Bofors cannon but no 7.62 mm close support armament. The Surprise Package configuration served as a test bed for the avionic systems and armament for the AC-130E. In 1970, ten more AC-130As were acquired under the “Pave Pronto” project.[12] In the summer of 1971, Surprise Package AC-130s were converted to the Pave Pronto configuration and assumed the new nickname of ‘Thor’. Conversion of C-130Es into AC-130Es for the “PAVE Spectre” project followed.[13][14] Regardless of their project names the aircraft were more commonly referred to by the squadron’s call sign ‘Spectre’.

Recent and planned upgrades

 
AC-130U armed with two 30 mm Bushmasters, 2007

In 2007, Air Force Special Operations Command (AFSOC) initiated a program to upgrade the armament of AC-130s. The test program planned for the 25 mm GAU-12/U and 40 mm Bofors cannon on the AC-130U gunships to be replaced with two 30 mm Mk 44 Bushmaster II cannons.[15] In 2007, the Air Force modified four AC-130U gunships as test platforms for the Bushmasters. These were referred to as AC-130U Plus 4 or AC-130U+4. AFSOC, however, canceled its plans to install the new cannons on its fleet of AC-130Us. It has since removed the guns and re-installed the original 40 mm and 25 mm cannons and returned the planes to combat duty.[16] Brigadier General Bradley A. Heithold, AFSOC’s director of plans, programs, requirements, and assessments, said on 11 August 2008 that the effort was canceled because of problems with the Bushmaster’s accuracy in tests “at the altitude we were employing it”. There were also schedule considerations that drove the decision, he said.[17]

There were also plans to possibly replace the 105 mm cannon with a breech-loading 120 mm M120 mortar, and to give the AC-130 a standoff capability using either the AGM-114 Hellfire missile, the Advanced Precision Kill Weapon System (based on the Hydra 70 rocket), or the Viper Strike glide bomb.[18]

In 2010, the Air Force awarded L-3 Communications a $61 million contract to add precision strike packages to eight MC-130W Combat Spear special-mission aircraft[19] to give them a gunship-like attack capability; such-equipped MC-130Ws are known as Dragon Spears. Air Force Special Operations Command is arming these aircraft to relieve the high operational demands on AC-130 gunships until new AC-130Js enter service.[20] The MC-130W Dragon Spear was renamed the AC-130W Stinger II in 2011.[21] The precision strike packages consist of a 30 mm gun and several precision guided munitions (PGMs). Rails are mounted on the out-board pylon of the wing for four Hellfire missiles, SDBs, or SDB IIs under each. 10 Common Launch Tubes (CLTs) are mounted on the rear ramp to fire Griffin A missiles; additional missiles are stored in the aircraft that can be reloaded in flight.[22] CLTs are able to fire other small munitions able to fit inside the 6 in (15 cm)-diameter, 48 in (1.2 m)-long tubes.[23]

The Air Force launched an initiative in 2011 to acquire 16 new gunships based on new-built MC-130J Combat Shadow II special operations tankers outfitted with a “precision strike package” to give them an attack capability, requesting $1.6 billion from Fiscal Years 2011 through 2015. This would increase the size of the gunship fleet to 33 aircraft, a net increase of eight after the planned retirement of eight aging AC-130Hs. The first aircraft would be bought in Fiscal 2012, followed by two in Fiscal 2013, five in Fiscal 2014, and the final eight in Fiscal 2015.[24] The decision to retain the C-130 came after funding for 16 C-27Js was removed from the fiscal 2010 budget.[25] The AC-130J will follow the path of the Dragon Spear program.[26] On 9 January 2013, the Air Force began converting the first MC-130J Combat Shadow II into an AC-130J Ghostrider[27] and delivered it to AFSOC on 29 July 2015.[28] The first AC-130J is to enter service in 2017.[29]

The Air Force decided to add a 105 mm cannon to the AC-130J in addition to the 30 mm cannon and smart bombs, the shells being more accurate and cheaper than dropping SDBs. AFSOC is interested in adding a directed energy weapon to the AC-130J by 2020,[30] similar to the previous Advanced Tactical Laser program. It is to produce a beam of up to 120 kW, or potentially even 180–200 kW, weigh about 5,000 lb (2,300 kg), defensively destroy anti-aircraft missiles, and offensively engage communications towers, boats, cars, and aircraft.[31][32][33] However, laser armament may only be installed on a few aircraft rather than the entire AC-130J fleet;[34] the laser will be mounted on the side in place of the 30 mm cannon.[35] Other potential additions include an active denial system to perform airborne crowd control, and small unmanned aerial vehicles from the common launch tubes to provide remote video feed and coordinates to weapons operators through cloud cover.[36] Called the Tactical Off-board Sensor (TOBS), the drones would be expendable and fly along a pre-programed orbit to verify targets the aircraft can’t see itself because of bad weather or standing off from air defenses.[33][34] AFSOC will initially utilize the Raytheon Coyote small UAV for the TOBS mission, as it is an off-the-shelf design with a one-hour endurance, but plans to fulfill the role with a new drone capable of a four-hour endurance by 2019.[23]

The Air Force is also interested in acquiring a glide bomb that can be launched from the common launch tubes capable of hitting ground vehicles traveling as fast as 120 km/h (70 mph) while above 10,000 ft (3,000 m).[37] In June 2016, Dynetics was awarded a contract by SOCOM to integrate its tactical munition onto the AC-130. Designated the GBU-69/B Small Glide Munition, the weapon weighs 27 kg (60 lb) and is armed with a 16 kg (35 lb) blast-fragmentation warhead that can detonate by direct impact or at a pre-selected height; despite being smaller, being unpowered allows more volume for its warhead to be heavier than those on the Hellfire and Griffin A missiles, 9 kg (20 lb) and 5.9 kg (13 lb) respectively. Guidance is provided by a GPS receiver with anti-spoofing software and four Distributed Aperture Semi-Active Laser Seeker (DASALS) apertures adapted from the WGU-59/B APKWS for terminal guidance. Fielding is planned in 2017.[38][39][40]

Future

By 2018, AC-130 gunships will have been providing close air support for special operators for 50 years. Although the aircraft have been kept relevant through constant upgrades to their weaponry, sensor packages, and countermeasures, they are not expected to be survivable in future non-permissive environments due to their high signatures and low airspeeds. Military analysts, such as the Center for Strategic and Budgetary Assessments, have suggested that AFSOC invest in more advanced technologies to fill the role to operate in future contested combat zones, including a mix of low-cost disposable unmanned and stealthy strike aircraft.[41]

Design

 
Underside of an AC-130U Spooky

Overview

The AC-130 is a heavily armed long-endurance aircraft carrying an array of anti-ground oriented weapons that are integrated with sophisticated sensors, navigation, and fire-control systems. It is capable of delivering precision firepower or area-saturation fire over a target area over a long period of time, at night or in adverse weather. The sensor suite consists of a television sensor, infrared sensor, and radar. These sensors allow the gunship to visually or electronically identify friendly ground forces and targets in most weather conditions.

The AC-130U is equipped with the AN/APQ-180, a synthetic aperture radar for long-range target detection and identification. The gunship’s navigational devices include inertial navigation systems and a Global Positioning System. The AC-130U employs technologies developed in the 1990s which allow it to attack two targets simultaneously. It has twice the munitions capacity of the AC-130H.[3] Although the AC-130U conducts some operations in daylight, most of its combat missions are conducted at night.[42] The AC-130H’s unit cost is US$132.4 million, and the AC-130U’s cost is US$190 million (fiscal 2001 dollars).[6]

Upgrades

 
AC-130U sensor suite

During the Vietnam era, the various AC-130 versions following the Pave Pronto modifications were equipped with a magnetic anomaly detector system called Black Crow (designated AN/ASD-5), a highly sensitive passive device with a phased-array antenna located in the left-front nose radome that could pick up localized deviations in the Earth’s magnetic field normally used to detect submerged submarines. The Black Crow system was slaved into the targeting computers of the AC-130A/E/H, enabling the detection of the unshielded ignition coils of North Vietnamese trucks hidden under dense jungle foliage along the Ho Chi Minh trail. It could also detect hand-held transmitter signals of air controllers on the ground to identify and locate targets.

The PGM-38/U enhanced 25 mm high explosive incendiary round was created to expand the AC-130U gunships’ mission in standoff range and survivability for its 25 mm GAU-12/U gun. This round is a combination of the existing PGU-25 HEI and a M758 fuze designated as FMU-151/B to meet the MIL-STD-1316. The FMU-151 has an improved arming delay with multi-sensitive range.[43]

Operational history

Vietnam War

 
An AC-130 in Southern Laos circa 1970

The AC-130 gunship first arrived in South Vietnam on 21 September 1967 under the Gunship II program and began combat operations over Laos and South Vietnam that year. In June 1968, AC-130s were deployed to Tan Son Nhut AB near Saigon for support against the Tet Offensive. By 30 October 1968, enough AC-130 Gunship IIs arrived to form a squadron, the 16th Special Operations Squadron (SOS) of the 8th Tactical Fighter Wing (TFW), at Ubon Royal Thai Air Force Base, Thailand. It was at this time that the C-130A gunship was designated the AC-130A.

On 18 August 1968, an AC-130 gunship flying an armed reconnaissance mission in Vietnam’s III Corps was diverted to support the Katum Special Forces Camp. The ground commander quickly assessed the accurate fire and capabilities of this weapon system and called for fire on his own perimeter when the Viet Cong attempted to bridge the wire on the west side of his position.

By December 1968, most AC-130s flew under F-4 Phantom II escort (to protect the gunship against heavy and concentrated AAA fire) from the 497th Tactical Fighter Squadron, normally three Phantoms per Gunship. On 24 May 1969, the first Spectre gunship was lost to enemy fire.[44]

In late 1969, under code name “Surprise Package”, 56-0490 arrived with solid-state laser-illuminated low-light-level-TV with a companion YAG laser designator, an improved forward looking infrared (FLIR) sensor, video recording for TV and FLIR, an inertial navigation system, and a prototype digital fire control computer. The remaining AC-130s were refitted with upgraded similar equipment in the summer of 1970, and then redeployed to Ubon RTAFB. On 25 October 1971, the first “Cadillac” gunship, the AC-130E arrived in Vietnam. On 17 February 1972, the first 105 mm cannon arrived for service with Spectre and was installed on Gunship 570. It was used from mid-February until the aircraft received battle damage to its right flap. The cannon was switched to Gunship 571 and was used until 30 March when the aircraft was shot down.

Summary of AC-130 Spectre gunships lost in the Vietnam War 1969–1972
Date Gunship model Unit Cause of loss / remarks
24/05/69 AC-130A 16th Special Operations Squadron (SOS) Downed by 37 mm anti-aircraft artillery (AA) at 6,500 feet while on reconnaissance for enemy trucks.[45]
22/04/70 AC-130A 16th SOS Downed while truck hunting by 37 mm AA[46]
28/03/72 AC-130A 16th SOS Downed while truck hunting along the Ho Chi Minh Trail by a SA-2 surface-to-air missile (SAM). Nose art named “Prometheus“.[47]
30/03/72 AC-130E 16th SOS Downed while truck hunting by 57 mm AA at 7,500 feet. The “E” model was armed with a 105 mm howitzer. This search and rescue (SAR) mission was “overshadowed by the Bat-21 rescue mission.”[48]
18/06/72 AC-130A 16th SOS Downed by a SA-7 shoulder fired SAM which struck the #3 engine and blew off the wing.[49]
21-22/12/72 AC-130A 16th SOS Downed while truck hunting along the Ho Chi Minh trail at 7,800 feet by 37 mm AA.[50]

On 28 January 1973, the Vietnam peace accord went into effect, marking the end of Spectre operations in Vietnam. Spectre was still needed and active in the region, supporting operations in Laos and Cambodia. On 22 February 1973, American offensive operations in Laos ended and the gunships became totally committed to operations in the Cambodian conflict.

On 12 April 1975, the Khmer Rouge were threatening the capital of Phnom Penh and AC-130s were called on to help in Operation Eagle Pull, the final evacuation of American and allied officials from Phnom Penh before it fell to the communists. The AC-130 was also over Saigon on 30 April 1975 to protect the final evacuation in Operation Frequent Wind. Spectres were also called in when the SS Mayaguez was seized, on the open sea, by Khmer Rouge soldiers and sailors on 15 May 1975.

Six AC-130s and 52 air crew members were lost during the war.[44] AC-130s destroyed more than 10,000 trucks and participated in many crucial close air support missions in Vietnam.

Cold War and later action

 
AC-130A performs a left-hand pylon turn

With the conclusion of hostilities in Southeast Asia in the mid-1970s, the AC-130H became the sole gunship in the regular Air Force, home based at Hurlburt Field, Florida, while the AC-130A fleet was transferred to the Air Force Reserve‘s 919th Tactical Airlift Group (919 TAG) at Eglin AFB Auxiliary Field #3/Duke Field, Florida. With the transition to the AC-130A, the 919 TAG was then redesignated as the 919th Special Operations Group (919 SOG).

In the late 1970s, when the AC-130H fleet was first being modified for in-flight refueling capability, a demonstration mission was planned and flown from Hurlburt Field, Florida, non-stop, to conduct a 2-hour live-fire mission over Empire Firing Range in the Republic of Panama, then return home. This 13-hour mission with two in-flight refuelings from KC-135 tankers proved the validity of flying long-range missions outside the contiguous United States to attack targets then return to home base without intermediate stops.

AC-130s from both the 4th and 16th Special Operations Squadrons have been deployed in nearly every conflict the United States has been involved in, officially and unofficially, since the end of the Vietnam War.

In July 1979, AC-130H crews deployed to Howard Air Force Base, Panama, as a precaution against possible hostile actions against American personnel during the Nicaraguan Revolution. New time aloft and non-stop distance records were subsequently set by a 16th SOS 2-ship AC-130H formation flight that departed Hurlburt Field on 13 November 1979 and landed on 15 November at Andersen Air Force Base, Guam, a distance of 7,200 nautical miles (13,300 km) and 29 hours 43 minutes non-stop, refueling four times in-flight.[51][52] Refueling support for the Guam deployment was provided by KC-135 crews from the 305th Air Refueling Wing from Grissom AFB, Indiana.

In November 1979, four AC-130H gunships flew nonstop from Hurlburt Field to Anderson AFB, Guam, because of the hostage situation at the Embassy in Iran. At Guam, AC-130H crews developed communications-out/lights-out refueling procedures for later employment by trial-and-error. This deployment with the 1 SOW/CC as Task Force commander was directed from the office of the CJCS for fear that Iranian militants could begin executing American Embassy personnel who had been taken hostage on 4 November. One early option considered AC-130H retaliatory punitive strikes deep within Iran. Later gunship flights exceeded the 1979 Hurlburt-to-Guam flight. Upon return in March 1980, the four planes soon found themselves in Egypt to support the ill-fated hostage rescue attempt.

 
Smoke visible from Gatling gun during twilight operations in 1988

During Operation Urgent Fury in Grenada in 1983, AC-130s suppressed enemy air defense systems and attacked ground forces enabling the assault of the Point Salines Airfield via airdrop and air-land of friendly forces. The AC-130 aircrew earned the Lieutenant General William H. Tunner Award for the mission.

The AC-130Hs of the 16th Special Operations Squadron unit maintained an ongoing rotation to Howard AB, Panama, monitoring activities in El Salvador and other Central American points of interest, with rules of engagement eventually permitting attacks on FMLN targets. This commitment of Maintainers and crews started in 1983 and lasted until 1990.[53] The AC-130 is considered to have hastened the end of the Salvadoran Civil War in the 1980s. Crews flew undercover missions from Honduras and attacked guerrilla camps and concentrations.[citation needed]

AC-130s also had a primary role during the United States invasion of Panama (named Operation Just Cause) in 1989, when they destroyed Panama Defense Force headquarters and numerous command-and-control facilities, and provided close air support for US ground troops. Aircrews earned the Mackay Trophy for the most meritorious flight of the year, and the Tunner Award.

Gulf War and the 1990s

Lockheed AC-130 in combat operation, USAF.

During the Gulf War of 1990–91 (Operations Desert Shield and Desert Storm), Regular Air Force and Air Force Reserve AC-130s provided close air support and force protection (air base defense) for ground forces, and battlefield interdiction. The primary interdiction targets were early warning/ground control intercept (EW/GCI) sites along the southern border of Iraq. At its standard altitude of 12,000 feet, the aircraft had a proven ability to engage moving ground targets.[54] The first gunship to enter the Battle of Khafji helped stop a southbound Iraqi armored column on 29 January 1991. One day later, three more gunships provided further aid to Marines participating in the operation. The gunships attacked Iraqi positions and columns moving south to reinforce their positions north of the city.

Despite the threat of surface-to-air missiles (SAMs) and increasing visibility during the early morning hours of 31 January 1991, one AC-130H, AF Serial No. 69-6567, call-sign Spirit 03, opted to stay to continue to protect the Marines. A lone Iraqi with a Strela-2 MANPADS shot Spirit 03 down, and all 14 crew members died.[55]

The military has used AC-130 gunships during the humanitarian operations in Somalia (Operation Restore Hope and Operation United Shield) in 1992–93, Operation Uphold Democracy in Haiti in 1994. AC-130s took part in Operation Assured Response in Liberia in 1996 and in Operation Silver Wake in 1997, the evacuation of American non-combatants from Albania.

AC-130s took part in the NATO missions in Bosnia and Herzegovina and Kosovo during the 1990s.

The AC-130U gunship set a new record for the longest sustained flight by any C-130 on 22 and 23 October 1997, when two AC-130U gunships flew 36 hours nonstop from Hurlburt Field, Florida to Taegu Air Base (Daegu), South Korea, being refueled seven times in the air by KC-135 tankers. The two gunships took on 410,000 lb (186,000 kg) of fuel. Gunships also were part of the buildup of U.S. forces in 1998 to compel Iraq to allow UNSCOM weapons inspections.

War on Terror

 
An AC-130U releasing flares

The U.S. has used gunships with deployments to the War in Afghanistan (Operation Enduring Freedom – Afghanistan) (2001–2014), and Iraq War (Operation Iraqi Freedom) (2003–11). AC-130 strikes were directed by special forces on known Taliban locations during the early days of the war in Afghanistan. U.S. Special Operations Forces are using the AC-130 to support its operations. The day after arriving in Afghanistan, the AC-130s attacked Taliban and Al-Qaeda forces near the city of Konduz and were directly responsible for the city’s surrender the next day. On 26 November 2001, Spectres were called in to put down a rebellion at the prison fort of Qala-I-Janghi. The 16 SOS flew missions over Mazar-i-Sharif, Kunduz, Kandahar, Shkin, Asadabad, Bagram, Baghran, Tora Bora, and virtually every other part of Afghanistan. The Spectre participated in countless operations within Afghanistan, performing on-call close air support and armed reconnaissance. In March 2002, three AC-130 Spectres provided 39 crucial combat missions in support of Operation Anaconda in Afghanistan. During the intense fighting, the planes fired more than 1,300 40 mm and 1,200 105 mm rounds.

Close air support was the main mission of the AC-130 in Iraq. Night after night, at least one AC-130 was in the air to fulfill one or more air support requests (ASRs). A typical mission had the AC–130 supporting a single brigade’s ASRs followed by aerial refueling and another two hours with another brigade or SOF team. The use of AC-130s in places like Fallujah, urban settings where insurgents were among crowded populations of non-combatants, was criticized by human rights groups. AC-130s were also used for intelligence gathering with their sophisticated long-range video, infrared and radar sensors. In 2007, US Special Operations forces also used the AC-130 in attacks on suspected Al-Qaeda militants in Somalia.[56][57]

There were eight AC-130H and seventeen AC-130U aircraft in active-duty service as of July 2010.[6] In March 2011, the U.S. Air Force deployed two AC-130U gunships to take part in Operation Odyssey Dawn, the U.S. military intervention in Libya,[58] which eventually came under NATO as Operation Unified Protector.[59]

External video
AC-130 Whiskey on YouTube from Deadliest Tech

By September 2013, 14 MC-130W Dragon Spear aircraft have been converted to AC-130W Stinger II gunships. The Stinger gunships have been deployed to Afghanistan to replace the aging AC-130H aircraft and provide an example for the new AC-130J Ghostrider. Modifications began with crews cutting holes in the plane to make room for weapons, and adding kits and bomb bases for laser-guided munitions. Crews added a 105 mm cannon, 20-inch infrared and electro-optical sensors, and the ability to carry 250-pound bombs on the wings.[60]

On 15 November 2015, two days after the attacks in Paris by ISIL, AC-130s and A-10 Thunderbolt II attack aircraft destroyed a convoy of over 100 ISIL-operated oil tanker trucks in Syria. The attacks were part of an intensification of the U.S.-led Military intervention against ISIL called Operation Tidal Wave II (named after the original Operation Tidal Wave during World War II, a failed attempt to raid German oil fields that resulted in heavy aircraft and aircrew loss) in an attempt to cut off oil smuggling as a source of funding for the group.[61]

The U.S. has continued to use the aircraft in the War in Afghanistan (2015–present).[62][63] On 3 October 2015, five attacks on a Doctors Without Borders hospital in Kunduz, Afghanistan were carried out by an AC-130.[64][65]

Variants

AC-130A Spectre (Project Gunship II, Surprise Package, Pave Pronto)

Conversions of C-130As; 19 completed; transferred to Air Force Reserve in 1975, retired in 1995.[12][66]

AC-130E Spectre (Pave Spectre, Pave Aegis)

Conversions of C-130Es; 11 completed; 10 upgraded to AC-130H configuration.[67]

AC-130H Spectre

Upgraded AC-130E aircraft; eight completed; last aircraft retired in 2015.[1]

AC-130U Spooky

Operational aircraft (active duty USAF); 17 in service.[68]

AC-130J Ghostrider[27]

Based on MC-130J; 32 aircraft to be procured to replace AC-130H.[69]

AC-130W Stinger II (former MC-130W Dragon Spear)

Conversions of MC-130Ws (active duty USAF).[70]

Operators

 
AC-130U over Hurlburt Field

 United States

United States Air Force[71][72][73]

16th Special Operations Squadron

4th Special Operations Squadron 2006 -

8th Special Operations Squadron 1975

16th Special Operations Squadron 1975 – 93, 2006-07

18th Flight Test Squadron 1991-93, 2006-

19th Special Operations Squadron 2006-

4th Special Operations Squadron 1995 – 2006

16th Special Operations Squadron

18th Flight Test Squadron

19th Special Operations Squadron 1996 – 2006

16th Special Operations Squadron

73d Special Operations Squadron

551st Special Operations Squadron

413th Flight Test Squadron

418th Flight Test Squadron

711th Special Operations Squadron

Aircraft on display

 
Nose art on AC-130A AF Serial No. 53-3129 at the USAF Armament Museum, Eglin AFB, Florida

One of the first seven AC-130A aircraft deployed to Vietnam was AF serial no. 53-3129, named First Lady in November 1970. This aircraft was a conversion of the first production C-130. On 25 March 1971, it took an anti-aircraft artillery hit in the belly just aft of the nose gear wheel well over the Ho Chi Minh trail in Laos. The 37 mm shell destroyed everything below the crew deck and barely missed striking two crew members. The pilot was able to crash land the aircraft safely.[74] In 1975, after the conclusion of US involvement in the Vietnam war, it was transferred to the Air Force Reserve, where it served with the 711th Special Operations Squadron of the 919th Special Operations Wing. In 1980, the aircraft was upgraded from the original three-bladed propellers to the quieter four-bladed propellers and was eventually retired in late 1995. The retirement also marked an end to the Air Force Reserve Command flying the AC-130A. The aircraft now sits on display in the final Air Force Reserve Command configuration with grey paint, black markings, and the four-bladed Hamilton Sunstrand 54H60-91 props at the Air Force Armament Museum at Eglin Air Force Base, Florida, USA.[75][76]

A second AC-130A, AF serial no. 56-0509, named the Ultimate End, was accepted by the Air Force on 28 February 1957, and modified to the AC-130A configuration on 27 July 1970. The aircraft participated in the Vietnam War and the rescue of the SS Mayaguez. Ultimate End demonstrated the durability of the C-130 after surviving hits in five places by 37 mm anti-aircraft artillery on 12 December 1970, extensive left wing leading edge damage on 12 April 1971 and a 57 mm round damaging the belly and injuring one crewman on 4 March 1972. “Ultimate End” was reassigned to the Air Force Reserve‘s 919th Special Operations Wing at Eglin AFB Auxiliary Field No.3 / Duke Field on 17 June 1975, where it continued in service until retired in the fall 1994 and transferred to Air Force Special Operations Command‘s Heritage Air Park at Hurlburt Field, Florida. While assigned to the 711th Special Operations Squadron, Ultimate End served in Operations JUST CAUSE in Panama, DESERT STORM in Kuwait and Iraq, and UPHOLD DEMOCRACY in Haiti. After 36 years and seven months of service, 24 years as a gunship, Ultimate End retired from active service on 1 October 1994. It made its last flight from Duke Field to Hurlburt Field on 20 October 1994. The Spectre Association dedicated “Ultimate End” (which served with the 16 SOS in Vietnam) on 4 May 1995. Lt Col Michael Byers, then 16 SOS commander, represented the active-duty gunship force and Clyde Gowdy of the Spectre Association represented all Spectre personnel past and present for the unveiling of a monument at the aircraft and the dedication as a whole.[77]

A third AC-130A, AF serial no. 54-1630, is on display in the Cold War Gallery at the National Museum of the United States Air Force at Wright-Patterson AFB, Ohio. Named Azrael for the angel of death in Islam who severs the soul from the body, this aircraft figured prominently in the closing hours of Operation Desert Storm. On 26 February 1991, Coalition ground forces were driving the Iraqi Army out of Kuwait. With an Air Force Reserve crew called to active duty, Azrael was sent to the Al Jahra highway (Highway 80) between Kuwait City and Basra, Iraq, to intercept the convoys of tanks, trucks, buses, and cars fleeing the battle. Facing SA-6 and SA-8 surface-to-air missiles and 37 mm and 57 mm radar-guided anti-aircraft artillery the crew attacked and destroyed or disabled most of the convoys. Azrael was also assigned to the 919th Special Operations Wing and retired to the museum in October 1995.[78]

Another AC-130A, AF serial no. 54-1626, the original prototype AC-130 named “Gunship II” is on display at the outdoor Air Park at the National Museum of the United States Air Force at Wright-Patterson AFB, Ohio.[79] This aircraft served in Southeast Asia from 1967 to 1972, then served in JC-130A test configuration. It was transferred to the National Museum of the United States Air Force in 1976, and converted back to AC-130A configuration in the late 1990s.

AC-130A serial no. 54-1623, c/n 3010, named “Ghost Rider” served in Southeast Asia and later conflicts until being retired in 1997 to Dobbins AFB, Georgia. Ghost Rider eventually was transferred and displayed at the Lockheed Museum at Marietta, Georgia.

Specifications

 
AC-130U Spooky

Data from USAF Fact Sheet[6]

General characteristics

  • Crew: 13

    • Officers: 5 (pilot, copilot, navigator, fire control officer, electronic warfare officer)
    • Enlisted: 8 (flight engineer, TV operator, infrared detection set operator, loadmaster, four aerial gunners)
  • Length: 97 ft 9 in (29.8 m)
  • Wingspan: 132 ft 7 in (40.4 m)
  • Height: 38 ft 6 in (11.7 m)
  • Wing area: 1745.5 ft² (162.2 m²)
  • Loaded weight: 122,400 lb (55,520 kg)
  • Max. takeoff weight: 155,000 lb (69,750 kg)
  • Powerplant: 4 × Allison T56-A-15 turboprops, 4,910 shp (3,700 kW) each

Performance

Armament

 
Gunners loading 40 mm cannon (background) and 105 mm cannon (foreground)

 
AC-130H Spectre over Santa Rosa Island, Northwest Florida coast.

AC-130A Project Gunship II

AC-130A Surprise Package, Pave Pronto, AC-130E Pave Spectre

  • 2× 7.62 mm GAU-2/A miniguns
  • 2× 20 mm M61 Vulcan cannon
  • 2× 40 mm (1.58 in) L/60 Bofors cannon

AC-130E Pave Aegis

  • 2× 20 mm M61 Vulcan cannon
  • 1× 40 mm (1.58 in) L/60 Bofors cannon
  • 1× 105 mm (4.13 in) M102 howitzer

AC-130H Spectre[80]

(Prior to c. 2000)

  • 2× 20 mm M61 Vulcan cannon
  • 1× 40 mm (1.58 in) L/60 Bofors cannon
  • 1× 105 mm (4.13 in) M102 howitzer

(Current Armament)

AC-130U Spooky II

AC-130W Stinger II / AC-130J Ghostrider[27]

Avionics

AC-130H Spectre

  • Mission systems:

    • Northrop Grumman AN/APN-241 multimode navigation radar – derived version of AN/APG-66 radar (formerly used on F-16A Fighting Falcon) consisting of precised navigation and air-to-ground modes including Monopulse Ground Mapping (MGM), Doppler Beam Sharpening (DBS), high resolution Synthetic Aperture Radar (SAR), Terrain Avoidance/Terrain Following (TA/TF), skin paint (for Station KEeping; SKE), maritime detection, weather/turbulence detection, wind shear alert, and ballistic wind measurement (for precision airdrop)[86]
    • Motorola (now General Dynamics) AN/APQ-150 Beacon Tracking Radar (BTR) – side-looking radar designed to search, acquire, and track ground beacon signal (X-band transponder) located at a friendly position from 10 nautical miles, beacon coordinate is used as a reference point for ground troop to give the gunship a bearing and range from the beacon to the desired target (mounted between 40 mm cannon and 105 mm howitzer)[87][88]
    • Cubic Corporation AN/ARS-6 Personnel Locator System (PLS) – radio navigation set[88]
    • Raytheon AN/AAQ-26 Infrared Detecting Set (IDS) – long-wave infrared (LWIR) band Forward Looking Infrared (FLIR) (mounted forward of the nose landing gear door)[88][89]
    • General Electric (now Lockheed Martin) AN/ASQ-145 Low Light Level Television (LLLTV) – EO fire control system consists of television camera (CCD-TV), AN/AVQ-19 Laser Target Designator/Ranger (LTD/R – 1064 nm laser emitter with permanently preset PRF code) with eyesafe mode (1570 nm laser emitter), AN/AAT-3 Ambient Temperature Illuminator (ATI – wide beam 860 nm laser illuminator), and Infrared Zoom Laser Illuminator Designator (IZLID – airborne version of 860 nm narrow beam laser pointer/marker and illuminator AN/PEQ-18) (mounted in the crew entrance door)[87][88]
  • Navigation systems:
  • Previously installed systems:
    • AN/APN-59 radar – search and weather radar[88]

AC-130U Spooky II

  • Mission systems:

    • Raytheon AN/APQ-180 multimode attack radar – enhanced version of AN/APG-70 radar (used on F-15E Strike Eagle) incorporating several enhanced air-to-ground modes such as fixed target track, ground moving target indication and track, projectile impact point position, beacon track, and a weather detection[88][90][91]
    • Raytheon AN/AAQ-26 IDS – LWIR FLIR (mounted on port side of the nose landing gear door)[88][89]
    • Lockheed Martin AN/AAQ-39 Gunship Multispectral Sensor System (GMS2) – EO/IR fire control system consists of mid-wave infrared (MWIR) FLIR, two Image-Intensified Television (I2TV) cameras (CCD-TV), laser target designator/rangefinder with eyesafe mode (1064 and 1570 nm dual mode laser emitter), and near-infrared (NIR) laser pointer/marker (860 nm laser emitter) (mounted under the nose of port landing gear sponson)[92]
  • Previously installed systems:
    • GEC-Marconi All Light Level Television (ALLTV) – EO fire control systems consists of CCD-TV, Laser Target Designator/Range Finder (LTD/RF – 1064 nm laser emitter with in-flight programmable PRF code) with eyesafe mode (1570 nm laser emitter), and Laser Illuminator Assembly (LIA – 860 nm laser emitter)[88]
  • Countermeasures:

Notable appearances in media

See also

Related development

Aircraft of comparable role, configuration and era

Related lists

References

  1.  
  1. Pike, John. “AC-130 Project Gunship II”. Global security. Retrieved 12 June 2013.

Further reading

External links

Wikimedia Commons has media related to AC-130 Spectre.

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Phalanx CIWS

From Wikipedia, the free encyclopedia
Phalanx CIWS

Phalanx (Block 1A) live fire test aboard USS Monterey in November 2008.
Type Close-in weapon system
Place of origin United States
Service history
In service 1980–present
Used by See operators
Wars Persian Gulf War
Production history
Designer General Dynamics (now Raytheon)
Manufacturer General Dynamics (now Raytheon)
Unit cost

5X Block 1B 8.56M pound to UK
9X Block 1B 13.66M USD each for SK
13 sets MK15 Phalanx Block 1B Baseline 2 for TW, 8 set is for upgrading the current Block 0 to MK15 Phalanx Block 1B Baseline 2, total cost: 0.416B with 260K MK 244 MOD 0 armor piercing bullet, Baseline2 is the newest model in Block 1B on 11/2016

(price may vary for different amounts of ammo, technical protocols, and personnel training)[1]

Produced 1978[2]
Specifications
Weight 12,500 lb (5,700 kg), later models 13,600 lb (6,200 kg)[2]
Barrel length • Block 0 & 1 (L76 gun barrel): 60 in (1,500 mm)
• Block 1B (L99 gun barrel): 78 in (2,000 mm)[3]
Height 15.5 ft (4.7 m)
Crew Automated, with human oversight

Shell • Naval: Armor-piercing tungsten penetrator rounds with discarding sabots.
• Land: High-Explosive Incendiary Tracer, Self-Destruct.
Caliber 20×102 mm
Barrels 6-barrel (progressive RH parabolic twist, 9 grooves)
Elevation • Block 0: -10°/+80°
• Block 1: -20°/+80°
(Rate of elevation: 86°/sec for Block 0/1)
• Block 1B: -25°/+85°
(Rate of elevation: 115°/sec)[3]
Traverse • 150° from either side of centerline
(Rate of traverse: 100°/sec for Block 0 & 1, 116°/sec for Block 1B)[3]
Rate of fire 4,500 rounds/minute (75 rounds/second).
Muzzle velocity 3,600 ft/s (1,100 m/s)[3]
Effective firing range Classified[2][4]
Maximum firing range 2.2 mi (3.5 km)[3]

Main
armament
1×20 mm M61 Vulcan 6-barreled Gatling cannon[5]
Guidance
system
Ku-band radar and FLIR[6]

The Phalanx CIWS (pronounced “sea-whiz”) is a close-in weapon system for defense against anti-ship missiles. It was designed and manufactured by the General Dynamics Corporation, Pomona Division[5] (now a part of Raytheon). Consisting of a radar-guided 20 mm Vulcan cannon mounted on a swiveling base, the Phalanx has been used by multiple navies around the world, notably the United States Navy on every class of surface combat ship with the exception of the San Antonio class LPD,[7] by the British Royal Navy in its older escorts (where weight limits the use of the heavier Dutch Goalkeeper 30 mm CIWS), by the United States Coast Guard aboard its Hamilton-class and Legend-class cutters, and the navies of 16 allied nations.

A land based variant, known as C-RAM, has recently been deployed in a short range missile defense role, to counter incoming rockets and artillery fire.[8]

Because of their distinctive barrel-shaped radome and their automated nature of operation, Phalanx CIWS units are sometimes nicknamed “R2-D2” after the famous droid character from the Star Wars films.[9][10]

Contents

History

The Phalanx Close-In Weapons System (CIWS) was developed as the last line of automated weapons defense (terminal defense or point defense) against anti-ship missiles (AShMs or ASMs) and attacking aircraft, including high-g and maneuvering sea-skimmers.

 
The Phalanx prototype on USS King in 1973.

The first prototype system was offered to the U.S. Navy for evaluation on the destroyer leader USS King in 1973 and it was determined that additional improvements were required to improve performance and reliability. Subsequently, the Phalanx Operational Suitability Model successfully completed its Operational Test and Evaluation (OT&E) on board the destroyer USS Bigelow in 1977. The model exceeded operational maintenance, reliability, and availability specifications. Another evaluation successfully followed, and the weapon system was approved for production in 1978. Phalanx production started with orders for 23 USN and 14 foreign military systems. The first ship fully fitted out was the aircraft carrier USS Coral Sea in 1980. The Navy began placing CIWS systems on non-combatant vessels in 1984.

Design

The basis of the system is the 20 mm M61 Vulcan Gatling gun autocannon, used since 1959 by the United States military on various tactical aircraft, linked to a Ku-band radar system for acquiring and tracking targets. This proven system was combined with a purpose-made mounting, capable of fast elevation and traverse speeds, to track incoming targets. An entirely self-contained unit, the mounting houses the gun, an automated fire-control system and all other major components, enabling it to automatically search for, detect, track, engage, and confirm kills using its computer-controlled radar system. Due to this self-contained nature, Phalanx is ideal for support ships, which lack integrated targeting systems and generally have limited sensors. The entire unit has a mass between 12,400 to 13,500 lb (5,600 to 6,100 kg).

Upgrades

 
Rounds from a Mk-15 Phalanx CIWS from the guided missile destroyer USS Mitscher impact ex-USNS Saturn during a sinking exercise (SINKEX), 2010.

Due to the continuing evolution of both threats and computer technology, the Phalanx system has, like most military systems, been developed through a number of different configurations. The basic (original) style is the Block 0, equipped with first-generation, solid-state electronics and with marginal capability against surface targets. The Block 1 (1988) upgrade offered various improvements in radar, ammunition, computing power, rate of fire, and an increase in maximum engagement elevation to +70 degrees. These improvements were intended to increase the system’s capability against emerging Russian supersonic anti-ship missiles. Block 1A introduced a new computer system to counter more maneuverable targets. The Block 1B PSuM (Phalanx Surface Mode, 1999) adds a forward-looking infrared (FLIR) sensor to make the weapon effective against surface targets.[11] This addition was developed to provide ship defense against small vessel threats and other “floaters” in littoral waters and to improve the weapon’s performance against slower low-flying aircraft. The FLIR’s capability is also of use against low-observability missiles and can be linked with the RIM-116 Rolling Airframe Missile (RAM) system to increase RAM engagement range and accuracy. The Block 1B also allows for an operator to visually identify and target threats.[11]

As the system model manager, the U.S. Navy is in the process of upgrading all their Phalanx systems to the Block 1B configuration. All U.S Navy Phalanx systems are scheduled for upgrade to Block 1B by the end of FY 2015. In addition to the FLIR sensor, the Block 1B incorporates an automatic acquisition video tracker, optimized gun barrels (OGB), and Enhanced Lethality Cartridges (ELC) for additional capabilities against asymmetric threats such as small maneuvering surface craft, slow-flying fixed and rotary-winged aircraft, and unmanned aerial vehicles. The FLIR sensor improves performance against anti-ship cruise missiles, while the OGB and ELC provide tighter dispersion and increased “first-hit” range; the Mk 244 ELC is specifically designed to penetrate anti-ship missiles with a 44-percent-heavier tungsten penetrator round and an aluminum nose piece. Another system upgrade is the Phalanx 1B Baseline 2 radar to improve detection performance, increase reliability, and reduce maintenance. It also has a surface mode to track, detect, and destroy threats closer to the water’s surface, increasing the ability to defend against fast-attack boats and low-flying missiles; the Baseline 2 radar upgrade is to be installed on all U.S. Navy Phalanx system-equipped vessels by FY 2019.[12] The Block 1B is also used by other navies, such as Canada, Portugal, Japan, Egypt, Bahrain, and the UK.[13]

US Navy Phalanx CIWS Maintenance & Live Firing Test

In April 2017, Raytheon tested a new electric gun for the Phalanx allowing the system to fire at varying rates to conserve ammunition. The new design replaces the pneumatic motor, compressor, and storage tanks, reducing system weight by 180 lb (82 kg) while increasing reliability and reducing operating costs.[14]

Operation

The CIWS is designed to be the last line of defense against anti-ship missiles. Due to its design criteria, its effective range is very short relative to the range of modern ASMs, from 1 to 5 nautical miles (9 km). The gun mount moves at a very high speed and with great precision. The system takes minimal inputs from the ship, making it capable of functioning despite potential damage to the ship. The only inputs required for operation are 440 V AC Three-phase electric power at 60 Hz and water (for electronics cooling). For full operation, including some non-essential functions, it also has inputs for true compass ship’s heading and 115 V AC for the PASS subsystem.

 
A technician checks the radar transmitter and microwave assemblies of a Phalanx CIWS, most likely a Block 0. On the unit in the background, the search radar can be seen at the top left with the vertical, orange-peel shaped, tracking radar below it.

Radar subsystems

The CIWS has two antennas that work together to engage targets. The first antenna, for searching, is located inside the radome on the weapon control group (top of the white-painted portion). The search subsystem provides bearing, range, velocity, heading, and altitude information of potential targets to the CIWS computer. This information is analyzed to determine whether the detected object should be engaged by the CIWS system. Once the computer identifies a valid target (see details below), the mount moves to face the target and then hands the target over to the tracking antenna. The track antenna is extremely precise, but views a much smaller area. The tracking subsystem observes the target until the computer determines that the probability of a successful hit is maximized and then, depending on the operator conditions, the system either fires automatically or recommends fire to the operator. While firing, the system tracks outgoing rounds and ‘walks’ them onto the target.

 
U.S. Navy sailors load tungsten ammunition (white sabots at right) and off-load dummy ammunition (left).

Gun and ammunition handling system

The Block 0 CIWS mounts (hydraulic driven) fired at a rate of 3,000 rounds per minute and held 989 rounds in the magazine drum.[5] The Block 1 CIWS mounts (hydraulic) also fired at 3,000 rounds per minute with an extended magazine drum holding 1,550 rounds. The Block 1A and newer (pneumatic driven) CIWS mounts fire at a rate of 4,500 rounds per minute with a 1,550-round magazine. The velocity of the rounds fired is approximately 3,600 feet per second (1,100 m/s). The rounds are armor-piercing tungsten penetrator rounds or depleted uranium with discarding sabots. The Phalanx CIWS 20 mm rounds are designed to destroy a missile’s airframe and make it unaerodynamic, thus keeping shrapnel from the exploding projectile to a minimum, effectively keeping collateral damage to a minimum. The ammunition handling system has two conveyor belt systems. The first takes the rounds out of the magazine drum to the gun; the second takes empty shells or non-fired rounds to the opposite end of the drum.

CIWS contact target identification

The CIWS does not recognize identification friend or foe, also known as IFF. The CIWS only has the data it collects in real time from the radars to decide if the target is a threat and to engage it. A contact must meet multiple criteria for the CIWS to consider it a target. These criteria include:

 
A sailor sits at a CIWS Local Control Panel (LCP) during a general quarters drill.
  1. Is the range of the target increasing or decreasing in relation to the ship? The CIWS search radar sees contacts that are out-bound and discards them. The CIWS engages a target only if it is approaching the ship.
  2. Is the contact capable of maneuvering to hit the ship? If a contact is not heading directly at the ship, the CIWS looks at its heading in relation to the ship and its velocity. It then decides if the contact can still perform a maneuver to hit the ship.
  3. Is the contact traveling between the minimum and maximum velocities? The CIWS has the ability to engage targets that travel in a wide range of speeds; however, it is not an infinitely wide range. The system has a target maximum-velocity limit. If a target exceeds this velocity, the CIWS does not engage it. It also has a target minimum-velocity limit, and does not engage any contact below that velocity. The operator can adjust the minimum and maximum limits within the limits of the system.

There are many other subsystems that together ensure proper operation, such as environmental control, transmitter, mount movement control, power control and distribution, and so on. It takes six to eight months to train a technician to maintain, operate, and repair the CIWS.

Incidents

Drone exercise catastrophic accidents

On 10 February 1983, USS Antrim was conducting a live-fire exercise off the East Coast of the United States using the Phalanx against a target drone. Although the drone was successfully engaged at close range, the target debris bounced off the sea surface and struck the ship. This caused significant damage and fire from the drone’s residual fuel, which also killed a civilian instructor aboard this ship.[15][16]

On 11 October 1989, USS El Paso was conducting a live-fire exercise off the East Coast of the United States using the Phalanx against a target drone. The drone was successfully engaged, but as the drone fell to the sea, the CIWS re-engaged it as a continued threat to El Paso. Rounds from the Phalanx struck the bridge of USS Iwo Jima, killing one officer and injuring a petty officer.[17]

Iraqi missile attack in 1991 Gulf War

On 25 February 1991, during the first Gulf War, the Phalanx-equipped frigate USS Jarrett was a few miles from the US battleship USS Missouri and the British destroyer HMS Exeter. The ships were thought to be under attack by an Iraqi Silkworm missile (often referred to as the Seersucker), at which time Missouri fired its SRBOC chaff. The Phalanx system on Jarrett, operating in the automatic target-acquisition mode, fixed on Missouri‘s chaff, releasing a burst of rounds. From this burst, four rounds hit Missouri, which was 2–3 miles (3.2–4.8 km) from Jarrett at the time. There were no injuries.[18] No missile had in fact been fired, the chaff firing was in response to an erroneous ‘missile firing alert’ that was actually an oil well head going up. The Iraqis had been setting the oil wells alight in Kuwait for some days. Exeter had relieved HMS Gloucester in the Northern Gulf a few days before and, in the weeks before that, Gloucester had taken out a Silkworm aimed at Missouri.

 
JMSDF mounted Phalanx CIWS

Accidental downing of US aircraft by the Japanese destroyer Yūgiri

On 4 June 1996, a Japanese Phalanx accidentally shot down a US A-6 Intruder from the aircraft carrier USS Independence that was towing a radar target during gunnery exercises about 1,500 miles west of the main Hawaiian island of Oahu. A Phalanx aboard the Asagiri-class destroyer JDS Yūgiri locked onto the Intruder instead of the target. Both the pilot and bombardier/navigator ejected safely.[19] A post-accident investigation concluded that Yūgiri‘s gunnery officer gave the order to fire before the A-6 was out of the CIWS engagement envelope.[20][21]

Centurion C-RAM

 
Centurion C-RAM

Seeking a solution to constant rocket and mortar attacks on bases in Iraq, the United States Army requested a quick-to-field anti-projectile system in May 2004, as part of its Counter-Rocket, Artillery, Mortar initiative.[22] The end result of this program was ‘Centurion’. For all intents and purposes, a terrestrial version of the Navy’s CIWS, the Centurion was rapidly developed,[23] with a proof-of-concept test in November that same year. It began deployment to Iraq in 2005,[22][24] where it was set up to protect forward operating bases and other high-value sites in and around the capital, Baghdad.[25] Israel has purchased a single system for testing purposes, and was reported[26] to have considered buying the system to counter rocket attacks and defend point military installations. However, the swift and effective development and performance of Israel’s indigenous Iron dome system has ruled out any purchase or deployment of Centurion.

Each system consists of a modified Phalanx 1B CIWS, powered by an attached generator and mounted on a trailer for mobility. Including the same 20 mm M61A1 Gatling gun, the unit is likewise capable of firing 4,500 20 mm rounds per minute.[8][27] In 2008, there were more than 20 CIWS systems protecting bases in the U.S. Central Command area of operations. A Raytheon spokesman told Navy Times that 105 attacks were defeated by the systems, most of those involved mortars. Based on the success of Centurion, 23 additional systems were ordered in September 2008.[28]

Like the naval (1B) version, Centurion uses Ku-band radar and FLIR[29] to detect and track incoming projectiles, and is also capable of engaging surface targets, with the system able to reach a minus-25-degree elevation.[29] The Centurion is reportedly capable of defending a 0.5 mi square area.[30] One major difference between the land- and sea-based variants is the choice of ammunition. Whereas naval Phalanx systems fire tungsten armor-piercing rounds, the C-RAM uses the 20 mm HEIT-SD (High-Explosive Incendiary Tracer, Self-Destruct) ammunition, originally developed for the M163 Vulcan Air Defense System.[23][31] These rounds explode on impact with the target, or on tracer burnout, thereby greatly reducing the risk of collateral damage should any rounds fail to hit their target.[23][31]

Operators

 
Map of Phalanx CIWS operators in blue

Specifications (Block 1A/B)

 
Raytheon Missile Systems Phalanx Block 1B close-in weapon system (CIWS) on board the Royal Navy Type 45 destroyer HMS Daring.
  • Gun: 1× 20 mm M61 Vulcan 6-barreled Gatling cannon[5]
  • Height: 15.5 ft (4.7 m)
  • Weight: 12,500 lb (5,700 kg), later models 13,600 lb (6,200 kg)[2]
  • Elevation −25° to +85°
  • Muzzle velocity: 3,600 ft/s (1,100 m/s)
  • Rate of fire: 4,500 rounds/minute
  • Maximum burst size: 1000 rounds
  • Ammunition capacity: 1,550 rounds
  • Radar: Ku band
  • 100% Kill distance: Classified
  • Cost: $3.8 Million[39]
  • Target Mach 2.[40]

Similar systems

References

Notes

  1.  

External links

Wikimedia Commons has media related to Phalanx CIWS.
 
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