GBU-15

Initial Operational Capability (IOC) : 1983
Total Production : ?

Model Status Year Produced
GBU-15()V1/B Retired - No Longer Operational 1983 ?
GBU-15()V2/B Retired - No Longer Operational 1985 ?
AGM-130A (TV) Active 1994 ?
AGM-130A (IR) Active 1994 ?
AGM-130C (TV) Active 1994 ?
AGM-130C (IR) Active 1994 ?
EGBU-15()V1/B Active 2000 1,200
EGBU-15()V2/B Active 2000 ?



GBU-15()V1/B

Group : Bombs
Status : Retired - No Longer Operational
Origin : United States of America
Contractor : Boeing
Initial Operational Capability (IOC) : 1983
Total Production : ?
Unitary Cost : USD $242,000

The GBU-15 is a combat-proven guided bomb capable of destroying the most hardened targets. During the Gulf War (1991) the GBU-15 demonstrated its capabilities against Saddam Hussein's regime. It was developed to be released from the F-111 and the F-4, currently is released from the F-15E Strike Eagle aircraft.

The GBU-15 consists of modular components attached to either a Mk 84 general purpose bomb or BLU-109 penetrating warhead. Each GBU-15 has a forward guidance section, warhead adapter section, control module, airfoil components and a weapon data link. The weapon can attack using the direct attack mode, which means the pilot locks the weapon onto the target and the GBU-15 guides itself to the target, and the indirect attack mode, which means the pilot must guide actively the GBU-15 bomb via the data-link to the selected target.

The GBU-15(V)1/B was deployed in 1983 and features a TV guidance system. During 1999 to 2000 a large number of GBU-15 bombs were upgraded to the EGBU-15 standard which adds a GPS/INS navigation unit for higher precision strikes. As of early 2011, the remaining EGBU-15 guided bombs are available for the F-15E aircraft with the GBU-15 model inventory being completely depleted.

Operators
Country Status State Notes
United States of AmericaRetired - No Longer Operational ?
Specifications
Notes
Dimensions
Diameter 460 millimeter
Length 3.9 meter
Wingspan 1.5 meter
Mass
Weight 2,500 pound
Performance
Max Launch Altitude 9,150 meter
Max Range 15 nautical mile
Min Range 5 nautical mile
Gear
Bombs
BLU-1091



GBU-15()V2/B

Group : Bombs
Status : Retired - No Longer Operational
Origin : United States of America
Contractor : Boeing
Initial Operational Capability (IOC) : 1985
Total Production : ?
Unitary Cost : USD $245,000

The GBU-15 is a combat-proven guided bomb capable of destroying the most hardened targets. During the Gulf War (1991) the GBU-15 demonstrated its capabilities against Saddam Hussein's regime. It was developed to be released from the F-111 and the F-4, currently is released from the F-15E Strike Eagle aircraft.

The GBU-15 consists of modular components attached to either a Mk 84 general purpose bomb or BLU-109 penetrating warhead. Each GBU-15 has a forward guidance section, warhead adapter section, control module, airfoil components and a weapon data link. The weapon can attack using the direct attack mode, which means the pilot locks the weapon onto the target and the GBU-15 guides itself to the target, and the indirect attack mode, which means the pilot must guide actively the GBU-15 bomb via the data-link to the selected target.

The GBU-15(V)2/B was deployed in 1985 and features an Infrared (IR) guidance system. During 1999 to 2000 a large number of GBU-15 bombs were upgraded to the EGBU-15 standard which adds a GPS/INS navigation unit for higher precision strikes. As of early 2011, the remaining EGBU-15 guided bombs are available for the F-15E aircraft with the GBU-15 model inventory being completely depleted.

Operators
Country Status State Notes
United States of AmericaRetired - No Longer Operational ?
Specifications
Notes
Dimensions
Diameter 460 millimeter
Length 3.9 meter
Wingspan 1.5 meter
Mass
Weight 1,134 kilogram
Performance
Max Launch Altitude 9,150 meter
Max Range 27,780 meter
Min Range 9,260 meter
Gear
Bombs
BLU-1091



AGM-130A (TV)

Group : Standoff Weapons
Status : Active
Origin : United States of America
Contractor : Boeing
Initial Operational Capability (IOC) : 1994
Total Production : ?
Unitary Cost : USD $450,000

The all-weather AGM-130 is an extended range derivative of the combat-proven GBU-15 bomb through the addition of a rocket motor and a new guidance package. The guidance system consists of an altimeter, GPS/INS-aided navigation system, and either an IR seeker or a CCD-TV seeker.

The seeker can be either locked onto the target before or after launch for automatic weapon guidance, or it can be manually steered by a weapon systems officer. Manual steering is performed through the two-way data link. The AGM-130 retains GBU-15 direct and indirect attack modes. The weapon can be dropped at high (direct and indirect modes) and low (indirect mode) altitude. The low altitude case is used to avoid enemy air defenses detection. Once the rocket motor is exhausted is ejected from the AGM-130 weapon.

The AGM-130 is designed for use in the F-15E Strike Eagle aircraft.

The AGM-130A features a Mk-84 blast/fragmentation warhead and a CCD-TV seeker.

Operators
Country Status State Notes
United States of AmericaActive ?
Specifications
Notes
Dimensions
Diameter 460 millimeter
Length 3.9 meter
Wingspan 1.5 meter
Mass
Weight 1,323 kilogram
Performance
Max Launch Altitude 9,150 meter
Max Range 75,000 meter
Min Range 9,260 meter



AGM-130A (IR)

Group : Standoff Weapons
Status : Active
Origin : United States of America
Contractor : Boeing
Initial Operational Capability (IOC) : 1994
Total Production : ?
Unitary Cost : USD $450,000

The all-weather AGM-130 is an extended range derivative of the combat-proven GBU-15 bomb through the addition of a rocket motor and a new guidance package. The guidance system consists of an altimeter, GPS/INS-aided navigation system, and either an IR seeker or a CCD-TV seeker.

The seeker can be either locked onto the target before or after launch for automatic weapon guidance, or it can be manually steered by a weapon systems officer. Manual steering is performed through the two-way data link. The AGM-130 retains GBU-15 direct and indirect attack modes. The weapon can be dropped at high (direct and indirect modes) and low (indirect mode) altitude. The low altitude case is used to avoid enemy air defenses detection. Once the rocket motor is exhausted is ejected from the AGM-130 weapon.

The AGM-130 is designed for use in the F-15E Strike Eagle aircraft.

The AGM-130A features a Mk-84 blast/fragmentation warhead and an Infrared IR seeker.

Operators
Country Status State Notes
United States of AmericaActive ?
Specifications
Notes
Dimensions
Diameter 460 millimeter
Length 3.9 meter
Wingspan 1.5 meter
Mass
Weight 1,323 kilogram
Performance
Max Launch Altitude 9,150 meter
Max Range 75,000 meter
Min Range 9,260 meter



AGM-130C (TV)

Group : Standoff Weapons
Status : Active
Origin : United States of America
Contractor : Boeing
Initial Operational Capability (IOC) : 1994
Total Production : ?
Unitary Cost : USD $450,000

The all-weather AGM-130 is an extended range derivative of the combat-proven GBU-15 bomb through the addition of a rocket motor and a new guidance package. The guidance system consists of an altimeter, GPS/INS-aided navigation system, and either an IR seeker or a CCD-TV seeker.

The seeker can be either locked onto the target before or after launch for automatic weapon guidance, or it can be manually steered by a weapon systems officer. Manual steering is performed through the two-way data link. The AGM-130 retains GBU-15 direct and indirect attack modes. The weapon can be dropped at high (direct and indirect modes) and low (indirect mode) altitude. The low altitude case is used to avoid enemy air defenses detection. Once the rocket motor is exhausted is ejected from the AGM-130 weapon.

The AGM-130 is designed for use in the F-15E Strike Eagle aircraft.

The AGM-130C features a BLU-109 penetration warhead and a CCD-TV seeker.

Operators
Country Status State Notes
United States of AmericaActive ?
Specifications
Notes
Dimensions
Diameter 460 millimeter
Length 3.9 meter
Wingspan 1.5 meter
Mass
Weight 1,323 kilogram
Performance
Max Launch Altitude 9,150 meter
Max Range 75,000 meter
Min Range 9,260 meter
Gear
Bombs
BLU-1091



AGM-130C (IR)

Group : Standoff Weapons
Status : Active
Origin : United States of America
Contractor : Boeing
Initial Operational Capability (IOC) : 1994
Total Production : ?
Unitary Cost : USD $450,000

The all-weather AGM-130 is an extended range derivative of the combat-proven GBU-15 bomb through the addition of a rocket motor and a new guidance package. The guidance system consists of an altimeter, GPS/INS-aided navigation system, and either an IR seeker or a CCD-TV seeker.

The seeker can be either locked onto the target before or after launch for automatic weapon guidance, or it can be manually steered by a weapon systems officer. Manual steering is performed through the two-way data link. The AGM-130 retains GBU-15 direct and indirect attack modes. The weapon can be dropped at high (direct and indirect modes) and low (indirect mode) altitude. The low altitude case is used to avoid enemy air defenses detection. Once the rocket motor is exhausted is ejected from the AGM-130 weapon.

The AGM-130 is designed for use in the F-15E Strike Eagle aircraft.

The AGM-130C uses a BLU-109 penetration warhead and an Infrared (IR) seeker.

Operators
Country Status State Notes
United States of AmericaActive ?
Specifications
Notes
Dimensions
Diameter 460 millimeter
Length 3.9 meter
Wingspan 1.5 meter
Mass
Weight 1,323 kilogram
Performance
Max Launch Altitude 9,150 meter
Max Range 75,000 meter
Min Range 9,260 meter
Gear
Bombs
BLU-1091



EGBU-15()V1/B

Group : Bombs
Status : Active
Origin : United States of America
Contractor : Boeing
Initial Operational Capability (IOC) : 2000
Total Production : 1,200
Unitary Cost : USD $242,000

The GBU-15 is a combat-proven guided bomb capable of destroying the most hardened targets. During the Gulf War (1991) the GBU-15 demonstrated its capabilities against Saddam Hussein's regime. It was developed to be released from the F-111 and the F-4, currently is released from the F-15E Strike Eagle aircraft.

The GBU-15 consists of modular components attached to either a Mk 84 general purpose bomb or BLU-109 penetrating warhead. Each GBU-15 has a forward guidance section, warhead adapter section, control module, airfoil components and a weapon data link.

The weapon can attack using the direct attack mode, which means the pilot locks the weapon onto the target and the GBU-15 guides itself to the target, and the indirect attack mode, which means the pilot must guide actively the GBU-15 bomb via the data-link to the selected target.

The EGBU-15 adds a GPS/INS guidance package to the GBU-15 bomb to achieve all-weather capability and unprecedented accuracy of about 3 meters CEP. The US Air Force plans to procure 1,200 EGBU-15 for the F-15E Strike Fighter fleet.

Operators
Country Status State Notes
United States of AmericaActive ?
Specifications
Notes
Dimensions
Diameter 460 millimeter
Length 3.9 meter
Wingspan 1.5 meter
Mass
Weight 1,134 kilogram
Performance
CEP 3 meter
Max Launch Altitude 9,150 meter
Max Range 27,780 meter
Min Range 9,260 meter
Gear
Bombs
BLU-1091



EGBU-15()V2/B

Group : Bombs
Status : Active
Origin : United States of America
Contractor : Boeing
Initial Operational Capability (IOC) : 2000
Total Production : ?
Unitary Cost : USD $245,000

The GBU-15 is a combat-proven guided bomb capable of destroying the most hardened targets. During the Gulf War (1991) the GBU-15 demonstrated its capabilities against Saddam Hussein's regime. It was developed to be released from the F-111 and the F-4, currently is released from the F-15E Strike Eagle aircraft.

The GBU-15 consists of modular components attached to either a Mk 84 general purpose bomb or BLU-109 penetrating warhead. Each GBU-15 has a forward guidance section, warhead adapter section, control module, airfoil components and a weapon data link.

The weapon can attack using the direct attack mode, which means the pilot locks the weapon onto the target and the GBU-15 guides itself to the target, and the indirect attack mode, which means the pilot must guide actively the GBU-15 bomb via the data-link to the selected target.

The EGBU-15 adds a GPS/INS guidance package to the GBU-15 bomb to achieve all-weather capability and unprecedented accuracy of about 3 meters CEP. The US Air Force plans to procure 1,200 EGBU-15 for the F-15E Strike Fighter fleet.

Operators
Country Status State Notes
United States of AmericaActive ?
Specifications
Notes
Dimensions
Diameter 460 millimeter
Length 3.9 meter
Wingspan 1.5 meter
Mass
Weight 1,134 kilogram
Performance
CEP 3 meter
Max Launch Altitude 9,150 meter
Max Range 27,780 meter
Min Range 9,260 meter
Gear
Bombs
BLU-1091

News

Wednesday, 8 August, 2007
Raytheon to Modify Weapons Data Link for F-15E Aircraft

INDIANAPOLIS, Aug. 8, 2007 /PRNewswire/ -- A subsidiary of Raytheon Company (NYSE: RTN) has been awarded a $75 million indefinite delivery-indefinite quantity contract

Photo Gallery

Notes

* Prime Contractor
State Latest Known holdings/Original Procurement
Com - Date of Commissioning
Decom - Date of Decommissioning

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