Generated by DeepSeek V3.2| GBU-38 Joint Direct Attack Munition | |
|---|---|
| Name | GBU-38 Joint Direct Attack Munition |
| Caption | A GBU-38 JDAM |
| Type | Precision-guided munition |
| Origin | United States |
| Service | 1998–present |
| Used by | United States Air Force, United States Navy, United States Marine Corps, and numerous allied nations |
| Designer | Boeing |
| Design date | 1990s |
| Manufacturer | Boeing |
| Production date | 1997–present |
| Variants | See #Variants |
| Weight | 500 lb (230 kg) |
| Length | 74.8 in (1.90 m) |
| Diameter | 14 in (360 mm) |
| Filling | Tritonal or H6 explosive |
| Filling weight | 192 lb (87 kg) |
| Guidance | Inertial navigation system integrated with GPS |
| Accuracy | <5 m CEP |
| Detonation | FMU-139 fuze |
| Wingspan | 25 in (640 mm) (tail fin span) |
GBU-38 Joint Direct Attack Munition. The GBU-38 is a precision-guided munition that converts an unguided, general-purpose Mk-82 500-pound bomb into a highly accurate, all-weather smart weapon. Developed by Boeing for the United States Department of Defense, it utilizes a GPS-aided inertial navigation system kit attached to the bomb's tail section. Entering service in the late 1990s, it has become a cornerstone of modern U.S. Air Force, Navy, and Marine Corps air-to-ground strike capabilities and is widely exported to allied nations.
The GBU-38 is a key member of the broader Joint Direct Attack Munition family, designed to provide a cost-effective method for achieving precise aerial bombardment. Its primary function is to strike high-value fixed or relocatable targets, such as command and control nodes, airfield structures, and armored vehicle concentrations, with minimal collateral damage. The weapon's guidance kit, consisting of a tail section with adjustable fins and a strake kit attached to the bomb body, interfaces with the launching aircraft's avionics for target coordinate programming. This design philosophy allows for the rapid conversion of vast existing inventories of dumb bombs into smart munitions, a concept heavily leveraged during operations like Operation Enduring Freedom and Operation Iraqi Freedom.
The JDAM program was initiated in the early 1990s by the United States Department of Defense to address the need for an affordable, all-weather precision strike capability following lessons learned from conflicts like the Gulf War. Boeing was selected as the prime contractor. The design centers on a modular guidance kit that can be fitted to various Mark 80 series bomb bodies; the GBU-38 specifically uses the Mk 82 general-purpose bomb. The kit integrates a GPS receiver with an inertial navigation system, providing guidance if GPS signals are degraded or jammed. Development and testing, involving entities like the Air Force Research Laboratory and Naval Air Warfare Center, proved successful, leading to full-rate production in 1997.
The GBU-38 achieved initial operational capability in 1998 and saw its first major combat use during NATO's Operation Allied Force in Kosovo. Its widespread deployment and effectiveness were decisively demonstrated in the War in Afghanistan (2001–2021) and the Iraq War, where it was employed extensively by aircraft like the F-16 Fighting Falcon, F/A-18 Hornet, and B-2 Spirit. The munition has been a staple in subsequent campaigns, including operations against the Islamic State of Iraq and the Levant in Syria and Iraq. Its use by international operators, such as the Royal Australian Air Force and the Israeli Air Force, further underscores its global adoption. The weapon's precision has been critical in urban combat environments, such as the Battle of Mosul.
The basic GBU-38 configuration has evolved into several specialized variants. The **GBU-38(V)1/B** incorporates a BLU-111 hardened bomb body. The **GBU-54 Laser JDAM** integrates a laser seeker with the GPS/INS guidance, allowing it to engage moving targets. Some variants feature different fuzing options, such as the FMU-152 Joint Programmable Fuze, for optimized effects. The fundamental JDAM guidance kit has also been applied to larger warheads, creating the GBU-31 (using the Mk 84 or BLU-109) and the GBU-32 (using the Mk 83), forming a complete family of scalable effects.
The GBU-38 uses a standard Mk 82 bomb body weighing approximately 500 pounds (230 kg). Its overall length is 74.8 inches (1.90 meters) with a body diameter of 14 inches (360 mm). The explosive fill is typically 192 pounds (87 kg) of Tritonal or H6 explosive, triggered by a FMU-139 or similar impact fuze. The attached guidance tail kit has a fin span of 25 inches (640 mm). It achieves a published circular error probable of less than 5 meters under ideal GPS conditions. The weapon can be released from altitudes above 15,000 feet and has a standoff range of several nautical miles, depending on release parameters.
Category:Precision-guided munitions of the United States Category:Bombs of the United States Category:Air-to-surface missiles