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Guided Bomb ยทLockheed Martin

GBU-16 Paveway II

The GBU-16 Paveway II is a laser-guided bomb, based on the Mk 83, used by the USAF, USN, and NATO for precision strikes. Key figures: weight 454 kg, warhead 202 kg, guidance Semi-active laser. In service with 14 countries โ€” Belgium, Denmark, France and 11 others.

Weight
454kg
Technical Specifications
WarheadMk 83 general-purpose bomb
Warhead weight202 kg (445 lb)
GuidanceSemi-active laser
Diameter356 mm (14.0 in)
Length3,700 mm (145.7 in)
Weight454 kg (1,001 lb)
CEP1 m
GBU-16 Paveway II scale diagram
GBU-16 Paveway II โ€” Guided Bomb 1.75 m 3.70 m
Weight
454 kg
Warhead
202 kg
Operators
๐Ÿ‡ง๐Ÿ‡ช Belgiumยท ๐Ÿ‡ฉ๐Ÿ‡ช Germanyยท ๐Ÿ‡ฉ๐Ÿ‡ฐ Denmarkยท ๐Ÿ‡ช๐Ÿ‡ธ Spainยท ๐Ÿ‡ซ๐Ÿ‡ท Franceยท ๐Ÿ‡ฌ๐Ÿ‡ง United Kingdomยท ๐Ÿ‡ฌ๐Ÿ‡ท Greeceยท ๐Ÿ‡ฎ๐Ÿ‡ณ Indiaยท ๐Ÿ‡ฎ๐Ÿ‡น Italyยท ๐Ÿ‡ฒ๐Ÿ‡พ Malaysiaยท ๐Ÿ‡ณ๐Ÿ‡ฑ Netherlandsยท ๐Ÿ‡ณ๐Ÿ‡ด Norwayยท ๐Ÿ‡น๐Ÿ‡ท Turkeyยท ๐Ÿ‡บ๐Ÿ‡ธ United States

Description

The GBU-16 Paveway II is an American laser-guided munition developed from a program initiated in 1964. The name Pave is an acronym for precision avionics vectoring equipment. The United States Air Force formalized the engineering effort under Project 3169 in 1967 to develop precision-guided munitions. This effort resulted in the Paveway I series, which was succeeded in the early 1970s by the Paveway II. The GBU-16 entered service around 1976.

The system consists of a Mk 83 general-purpose bomb modified with a laser seeker and wing assembly. Technical components include a semi-active laser seeker, a computer control group containing guidance and control electronics, a thermal battery, and a pneumatic control augmentation system. The munition utilizes front control canards and pop-out rear wings for stability and glide performance. Guidance is achieved by detecting reflected laser energy, or "sparkle," from a designating laser, which the seeker uses to actuate the canards. The control augmentation system employs "bang-bang" logic, commanding large canard deflections for course corrections, which results in a wobble during flight. This guidance method yields a circular error probability of 3.6 feet (1.1 m) for 99 deliveries, compared to 310 feet (94 m) for 99 unguided bombs dropped under similar conditions. Due to the energy expenditure caused by the control system's course corrections, the munition is typically released in a ballistic trajectory with the laser designator activated late in the flight to refine the impact point. The GBU-16 can be upgraded to the GBU-48 Enhanced Paveway II configuration through the addition of a GPS receiver, enabling dual-mode guidance and all-weather employment.

The munition is operated by the U.S. Air Force, U.S. Navy, U.S. Marine Corps, and various NATO air forces. It is integrated onto a wide range of platforms, including the F-15, F-16, F/A-18, F-35, and A-10, as well as international aircraft such as the Mirage 2000, Tornado, and Rafale. The weapon is also deployed on the MQ-9 Reaper unmanned aerial vehicle.

Wikipedia (CC BY-SA) and other open sources. Last updated on 28 April 2026. Suggest a change

Frequently Asked Questions

What type of weapon is the GBU-16 Paveway II?
The GBU-16 Paveway II is a guided bomb developed by Lockheed Martin. It entered service in 1976.
How much does the GBU-16 Paveway II weigh?
The GBU-16 Paveway II weighs 454 kg (1,000 lb), including a 202 kg warhead.
How is the GBU-16 Paveway II guided?
The GBU-16 Paveway II uses semi-active laser guidance.
Which countries use the GBU-16 Paveway II?
The GBU-16 Paveway II is in service with 14 countries: Belgium, Germany, Denmark, and 11 other countries.
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Latest Data Updates
  1. APR 282026 Updated Warhead weight updated
  2. APR 32026 Updated GBU-16 Paveway II: length added; GBU-16 Paveway II: diameter added
  3. MAR 302026 Created Page created: GBU-16 Paveway II