AGM-130 | |
---|---|
Type | Air-to-surface guided missile |
Place of origin | United States |
Service history | |
In service | 1994–2013 |
Used by | United States (USAF) |
Wars | Kosovo War |
Production history | |
Unit cost | Approximately $450,000 per weapon [1] |
Specifications | |
Mass | 2,917 lb (1,323 kg) |
Length | 12 feet, 10.5 inches (3.90 meters) [1] |
Diameter | 15 in/18 in (38 cm/46 cm) (bomb); 9 in (23 cm) (rocket motor) |
Wingspan | 59 in (150 cm) |
Warhead | 2,000 lb (907 kg) BLU-109 or MK 84 |
Operational range | 46.6 miles (75 kilometers) [2] although exact range is classified [1] |
Flight ceiling | 30,000-plus feet (9,100 meters) |
Maximum speed | High subsonic, [3] but exact speed is classified [1] |
The AGM-130 was an air-to-ground guided missile developed by the United States of America. Developed in 1984, it is effectively a rocket-boosted version of the GBU-15 bomb. It first entered operational service on 11 January 1999, and was retired in 2013. 502 were produced.
The AGM-130 is a powered air-to-surface missile designed for strikes at long range against various targets. It is essentially a rocket-boosted version of the GBU-15 bomb, [4] with the rocket motor increasing the launch range and so giving the launch aircraft protection from whatever defenses may protect the target. Two can be carried by the F-111 and F-15E.
In 1991 the development of some significant upgrades began; these included a new CCD seeker and a GPS/INS (GPS-aided Inertial Navigation System) mid-course guidance. This combined enhancement provided the system with an adverse weather capability. It can be retargeted in flight; the guidance head of the weapon provides a visual image of the target to the launch aircraft via the AXQ-14 data link, allowing the controller to steer it to the target (command guidance). The weapon can be retargeted in flight by simply steering it to a new target. Control can be released at any point, allowing the missile to home in on the target by itself. The AGM-130 is highly accurate, and is intended for use against high-value targets which are either slow moving or of fixed location.
The GBU-15 is a modular weapon, and the AGM-130 continues this concept. It consists of a CCD TV or focal plane array imaging infrared seeker head, a radar altimeter, wings, strakes, a Mark 84 or BLU-109 warhead, a control section, and a rocket motor and data link unit.
The AGM-130 needs little support on the ground, and can be based in remote "bare base" sites. What support and maintenance is required can be provided by mobile support equipment and intermediate level maintenance capability.
Development of the AGM-130A began in 1984 as an improvement to the GBU-15. The first unit became operational in 1994. [4] Precise numbers are classified, but the US Air Force planned to buy 4,000+ originally. This was reduced to 2,300 units, and in 1995 further reduced to 502.
Development of the AGM-130 cost $192 million, not including a further $11 million for the AGM-130C.
This section includes a list of references, related reading, or external links, but its sources remain unclear because it lacks inline citations .(April 2015) |
The upgraded AGM-130 Mid-Course Guidance (MCG) weapon, employs an improved global positioning and inertial navigation system. This allows the weapon to be used with less input from the launch aircraft, freeing the pilot and weapon systems officer for other tasks. The weapon became operational in 1999 when two F-15Es from the 335th and 336th Fighter Squadrons at Seymour Johnson Air Force Base, North Carolina, fired one weapon each.
The AGM-130LW [lightweight] is designed to be used by single-seat aircraft such as the F-16C. It also has an enhanced global positioning and inertial navigation system capability. The smaller, less powerful warhead used on this weapon allows better control over collateral damage.
The AGM-130C employed a 900 kg (2,000 lbs) BLU-109 penetrating warhead for use against hardened targets. It was developed, but not put into service.
The Autonomous AGM-130 is a proposed weapon that would incorporate a laser radar (LADAR) seeker, removing any need for the weapon to be steered to the target. The aircraft interface would be based on the JDAM interface; use of the autonomous seeker would greatly reduce the mission planning requirements and aircrew workload. Elimination of the datalink would also reduce the susceptibility to countermeasures.
The AGM-130 saw its first operational service on 11 January 1999 during Operation Northern Watch, when a pair of AGM-130s were used by F-15Es to destroy two Iraqi SAM sites. [5] The AGM-130 was also the weapon used in the April 1999 NATO strike on a railway bridge in Grdelica, Serbia.
The AGM-88 HARM is a tactical, air-to-surface anti-radiation missile designed to home in on electronic transmissions coming from surface-to-air radar systems. It was originally developed by Texas Instruments as a replacement for the AGM-45 Shrike and AGM-78 Standard ARM system. Production was later taken over by Raytheon Corporation when it purchased the defense production business of Texas Instruments.
The AGM-65 Maverick is an air-to-ground missile (AGM) designed for close air support. It is the most widely produced precision-guided missile in the Western world, and is effective against a wide range of tactical targets, including armor, air defenses, ships, ground transportation and fuel storage facilities.
A cruise missile is an unmanned self-propelled guided vehicle that sustains flight through aerodynamic lift for most of its flight path and whose primary mission is to place an ordnance or special payload on a target. Cruise missiles are designed to deliver a large warhead over long distances with high precision. Modern cruise missiles are capable of traveling at high subsonic, supersonic, or hypersonic speeds, are self-navigating, and are able to fly on a non-ballistic, extremely low-altitude trajectory.
The AGM-114 Hellfire is an American air-to-surface missile (ASM) first developed for anti-armor use, later developed for precision drone strikes against other target types, especially high-value targets. It was originally developed under the name "Heliborne laser, fire-and-forget missile", which led to the colloquial name "Hellfire" ultimately becoming the missile's formal name. It has a multi-mission, multi-target precision-strike ability and can be launched from multiple air, sea, and ground platforms, including the MQ-1 Predator and MQ-9 Reaper. The Hellfire missile is the primary 100-pound (45 kg) class air-to-ground precision weapon for the armed forces of the United States and many other nations. It has also been fielded on surface platforms in the surface-to-surface and surface-to-air roles.
The Rockwell International Guided Bomb Unit 15 is an unpowered glide weapon used to destroy high-value enemy targets. It was designed for use with F-15E Strike Eagle, F-111 'Aardvark' and F-4 Phantom II aircraft. The GBU-15 has long-range maritime anti-ship capability with the B-52 Stratofortress.
The Joint Direct Attack Munition (JDAM) is a guidance kit that converts unguided bombs, or "dumb bombs", into all-weather precision-guided munitions. JDAM-equipped bombs are guided by an integrated inertial guidance system coupled to a Global Positioning System (GPS) receiver, giving them a published range of up to 15 nautical miles (28 km). JDAM-equipped bombs range from 500 to 2,000 pounds. The JDAM's guidance system was jointly developed by the United States Air Force and United States Navy, hence the "joint" in JDAM. When installed on a bomb, the JDAM kit is given a GBU identifier, superseding the Mark 80 or BLU nomenclature of the bomb to which it is attached.
The McDonnell DouglasF-15E Strike Eagle is an American all-weather multirole strike fighter derived from the McDonnell Douglas F-15 Eagle. The F-15E was designed in the 1980s for long-range, high-speed interdiction without relying on escort or electronic-warfare aircraft. United States Air Force (USAF) F-15E Strike Eagles can be generally distinguished from other US Eagle variants by darker aircraft camouflage, conformal fuel tanks (CFTs) mounted along the engine intake ramps and a tandem-seat cockpit.
The AGM-154 Joint Standoff Weapon (JSOW) is a glide bomb that resulted from a joint venture between the United States Navy and Air Force to deploy a standardized medium range precision guided weapon, especially for engagement of defended targets from outside the range of standard anti-aircraft defenses, thereby increasing aircraft survivability and minimizing friendly losses. It is intended to be used against soft targets such as parked aircraft, trucks, armored personnel carriers (APCs), and surface-to-air missile sites (SAMs). Prior to launch, it is given a destination through either a predesignated waypoint or a point marked through a targeting pod. It glides, using two wings that pop out for added lift, to the marked destination and dispenses submunitions in a short, roughly linear pattern. The designation of the Joint Standoff Weapon as an "air-to-ground missile" is a misnomer, as it is an unpowered bomb with guidance avionics, similar to the older GBU-15.
The Boeing AGM-69 SRAM was a nuclear air-to-surface missile. It had a range of up to 110 nautical miles, and was intended to allow US Air Force strategic bombers to penetrate Soviet airspace by neutralizing surface-to-air missile defenses.
The AGM-86 ALCM is an American subsonic air-launched cruise missile (ALCM) built by Boeing and operated by the United States Air Force. This missile was developed to increase the effectiveness and survivability of the Boeing B-52H Stratofortress strategic bomber. The missile dilutes an enemy's forces and complicates air defense of its territory.
The AGM-12 Bullpup is a short-range air-to-ground missile developed by Martin Marietta for the US Navy. It is among the earliest precision guided air-to-ground weapons and the first to be mass produced. It first saw operational use in 1959 on the A-4 Skyhawk, but soon found use on the A-6 Intruder, F-100 Super Sabre, F-105 Thunderchief, F-4 Phantom II, F-8 Crusader, and P-3 Orion in both Navy and US Air Force service, as well as NATO allies. The weapon was guided manually via a small joystick in the aircraft cockpit, which presented a number of problems and its ultimate accuracy was on the order of 10 metres (33 ft), greater than desired. In the 1960s it was increasingly supplanted by fully automatic weapons like the AGM-62 Walleye and AGM-65 Maverick.
The AGM-78 Standard ARM was an anti-radiation missile developed by General Dynamics, United States. It was built on the airframe of the RIM-66 Standard surface-to-air missile, resulting in a very large weapon with considerable range, allowing it to attack targets as much as 50 miles (80 km) away.
The Popeye is a family of air-to-surface missiles developed and in use by Israel, of which several types have been developed for Israeli and export users. A long-range submarine-launched cruise missile variant of the Popeye Turbo has been speculated as being employed in Israel's submarine-based nuclear forces. The United States operated the Popeye under a different designation according to US naming conventions as the AGM-142 Have Nap.
The "SPICE" is an Israeli-developed, EO/GPS- guidance kit used for converting air-droppable unguided bombs into precision-guided bombs.
A guided bomb is a precision-guided munition designed to achieve a smaller circular error probable (CEP).
The GAM-63 RASCAL was a supersonic air-to-surface missile that was developed by the Bell Aircraft Company. The RASCAL was the United States Air Force's first nuclear armed standoff missile. The RASCAL was initially designated the ASM-A-2, then re-designated the B-63 in 1951 and finally re-designated the GAM-63 in 1955. The name RASCAL was the acronym for RAdar SCAnning Link, the missile's guidance system. The RASCAL project was cancelled in September 1958.
The AGM-176 Griffin is a lightweight, precision-guided munition developed by Raytheon. It can be launched from the ground or air as a rocket-powered missile or dropped from the air as a guided bomb. It carries a relatively small warhead, and was designed to be a precision low-collateral damage weapon for irregular warfare. It has been used in combat by the United States military during the War in Afghanistan.
A precision-guided munition (PGM), also called a smart weapon, smart munition, or smart bomb, is a guided munition intended to hit a specific target, to minimize collateral damage and increase lethality against intended targets. During the Persian Gulf War guided munitions accounted for only 9% of weapons fired, but accounted for 75% of all successful hits. Despite guided weapons generally being used on more difficult targets, they were still 35 times more likely to destroy their targets per weapon dropped.
The GBU-39/B Small Diameter Bomb (SDB) is a 250-pound (110 kg) precision-guided glide bomb that is intended to provide aircraft with the ability to carry a higher number of more accurate bombs. Most US Air Force aircraft will be able to carry a pack of four SDBs in place of a single 2,000-pound (910 kg) bomb. It first entered service in 2006. The Ground Launched Small Diameter Bomb (GLSDB) was later developed to enable the SDB to be launched from a variety of ground launchers and configurations.
The AGM-84H/K SLAM-ER is an advanced stand off precision-guided, air-launched cruise missile produced by Boeing Defense, Space & Security for the United States Armed Forces and their allies. Developed from the AGM-84E SLAM, the SLAM-ER is capable of attacking land and sea targets medium to long range. The SLAM-ER relies on the Global Positioning System (GPS) and infrared imaging for its navigation and control, and it can strike both moving and stationary targets.