Generated by DeepSeek V3.2| GBU-32 | |
|---|---|
| Name | GBU-32 |
| Caption | A GBU-32 Joint Direct Attack Munition. |
| Type | Precision-guided glide bomb |
| Origin | United States |
| Service | 1999–present |
| Used by | United States Navy, United States Air Force, Royal Australian Air Force, others |
| Designer | Boeing |
| Manufacturer | Boeing |
| Variants | See Variants |
| Weight | 1,000 lb (454 kg) |
| Length | 119.5 in (3.04 m) |
| Filling | Mk 83 general-purpose bomb or BLU-110 penetrator |
| Filling weight | 445 lb (202 kg) |
| Guidance | Inertial navigation system (INS) / Global Positioning System (GPS) |
| Wingspan | 63 in (1.6 m) (tail kit) |
GBU-32. The GBU-32 is a precision-guided Joint Direct Attack Munition (JDAM) kit that converts a standard 1,000-pound Mk 83 general-purpose bomb or a BLU-110 penetrator warhead into a highly accurate, all-weather smart weapon. Developed by Boeing for the United States Department of Defense, it entered service in the late 1990s and has been extensively used by the United States Navy and United States Air Force in multiple conflicts. The system uses a tail kit containing an Inertial navigation system (INS) and a Global Positioning System (GPS) receiver to guide the weapon to its target.
The GBU-32 is a key component of the Joint Direct Attack Munition family, providing a cost-effective method for achieving precision strikes. It is designed to be employed from various tactical aircraft, including the F/A-18 Hornet, F-15E Strike Eagle, and F-16 Fighting Falcon. The weapon's primary advantage is its ability to function accurately in adverse weather conditions where laser-guided systems may be ineffective. Operational use has demonstrated its reliability in engagements during Operation Enduring Freedom and Operation Iraqi Freedom, solidifying its role in modern U.S. military arsenals and those of allied nations like the Royal Australian Air Force.
The design of the GBU-32 centers on a modular tail kit produced by Boeing under contract from the United States Department of Defense. The kit integrates a Global Positioning System receiver with a hardened Inertial navigation system, allowing for continuous navigation updates after release from the launch aircraft. Development occurred during the 1990s as part of a broader effort to enhance the United States Air Force and United States Navy's all-weather strike capabilities following lessons from the Gulf War. The system mates with either the standard Mark 83 bomb or the hardened-target BLU-110 warhead, with guidance algorithms refined through testing at sites like Eglin Air Force Base.
The GBU-32 achieved initial operational capability in 1999 and saw its first major combat use during the NATO bombing of Yugoslavia. It became a weapon of choice during Operation Enduring Freedom in Afghanistan, where its GPS guidance proved invaluable for striking Taliban positions in mountainous terrain. Extensive use continued during Operation Iraqi Freedom, with aircraft from the USS Abraham Lincoln and USS Harry S. Truman employing it against Republican Guard facilities and command centers. The Royal Australian Air Force has also deployed the weapon in combat, including during operations against Islamic State of Iraq and the Levant targets in Syria.
The primary variants of the weapon are defined by their warhead and specific guidance enhancements. The standard GBU-32(V)1/B uses the Mark 83 bomb as its warhead. The GBU-32(V)2/B is configured with the BLU-110 penetrator for use against hardened or buried targets. Later developments include integration with the Joint Helmet Mounted Cueing System for improved targeting flexibility on platforms like the F-35 Lightning II. Some allied variants feature specific cryptographic or interface modifications for compatibility with international aircraft such as the Panavia Tornado used by the Royal Saudi Air Force.
The GBU-32 uses a 1,000-pound class warhead, either the Mark 83 bomb or the BLU-110. The complete weapon has a length of approximately 119.5 inches (3.04 meters) and a wingspan of 63 inches (1.6 meters) with the tail kit deployed. Guidance is provided by a hybrid Inertial navigation system and Global Positioning System receiver, with an estimated circular error probable of less than 5 meters under optimal conditions. The tail kit assembly contains control fins, a battery, and the guidance computer. The weapon is compatible with a wide range of United States military aircraft and can be released from altitudes above 15,000 feet and at significant standoff distances.
Category:Precision-guided munitions of the United States Category:Bombs of the United States Category:Joint Direct Attack Munition