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Classification groups of key explosive munitions used in conflicts

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The impact or effect the munition is intended to have

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Base Colour (12)

Colour of all, or some, of the markings on the munition

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Marking Script (9)

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Key features defining the operation mechanisms of a projectile

Mechanical Feature (10)

Whether a munition is guided or unguided

Guidance (2)

Munitions capable of altering their trajectory in flight
Guided Munition
Where the munition is launched from and what it targets

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The type of fins visible on the munition

Fins Characteristic (5)

The nominal diameter of a projectile. For most modern munitions, this is expressed in millimetres (e.g. 82 mm mortar projectile), but older artillery gun projectiles may be described in inches.

Calibre (72)

Weight class of the aerial bomb pictured

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Guided Munition
Munitions capable of altering their flight path in response to internal or external inputs, making them more precise. There are a range of ways munitions can be guided, including GPS, radar, and satellite, and guidance systems can be located in different parts of a munition.
OSMP832
Analyst Note:
This image shows the rear fin section that is attached to a M-302/Khaibar-1/Fadi series rockets to add guidance capabilities. This rear fin section is installed, along with a forward control section between the warhead and the rocket motor. The guided munition, now classified as a missile, is referred to as a Nasr-1/Nasr-2. A similar, but larger, rear fin section is fitted to Zelzal rockets to convert them to guided munitions. (ARES).
OSMP1252
Analyst Note:
This image shows several GBU-53/B bombs photographed from above while on a munitions transport cart. GBU-53/B bombs are transported and loaded onto the aircraft with the wing assembly on the bottom. When the GBU-53/B is released from the aircraft, the bomb rotates, with the wing assembly side orienting as the top as the bomb glides to its target. (ARES)
OSMP1248
Analyst Note:
This image shows a fragment of a RGM/UGM-109 Tomahawk Land Attack Missile (TLAM) series missile's WDU-36/B warhead. The WDU-36/B warhead is a penetrator warhead for the TLAM, and is one of several available warhead options for TLAM series missiles. The complete "WDU" designation isn't visible, but the part number (3123AS921) is associated with the WDU-36/B. (ARES)
OSMP805
Analyst Note:
This image shows the rocket motor of a Kheibar Shekan or Fattah-1 medium-range ballistic missile (MRBM). The Fattah-1 was publicly unveiled by Iran in June 2023, with very few images surfacing since that time. Due to the lack of available reference material, differentially identifying the Kheibar Shekan and Fattah-1 is difficult. The missile components displayed at unveilings and public displays are also often different from those used in production models. (ARES).
OSMP1177
Analyst Note:
This image shows the copper cone of the shaped charge located at the front of the warhead fitted to a Shahed-131. The Ukrainian armed forces have recorded that the cone measures 111 mm in diameter and 162 mm in depth. The warhead is lined with cubic pre-formed fragments of 7 mm in diameter. The explosive content of the warhead is estimated to be between 10 and 15 kg. (ARES)
OSMP1137
Analyst Note:
This image shows two MAM-L guided air-delivered bombs affixed to the wing of a Bayraktar TB2 drone. The MAM-L and TB2 are both produced in Türkiye by Roketsan and Baykar respectively. The MAM-L can have one of three different warheads: blast fragmentation, anti-tank, or thermobaric. The warhead section of each MAM-L in this image has “YIPE/BF” visible. ‘YIPE’ is the abbreviation of the warhead type in Turkish: Yüksek Infilaklı Parçacık Etkili (‘high explosive fragmentation’, in English). The ‘BF’ also indicates that these MAM-L munitions are of the blast-fragmentation variant. The warhead of a MAM-L cannot be determined from an external assessment without viewing markings such as these (or a clear view of the data plate, which can be seen on the aft portion of the MAM-L). (ARES)
OSMP1153
Analyst Note:
This image shows several remnants of a MAM-L bomb that are typically found after functioning. The actuated fins, as well as the fixed fins, are visible, along with various components of the control section that actuate the fins. The actuated fins attach to the control section, at the rear of the bomb, while the fixed fins attach to the middle of the bomb body. (ARES)
OSMP1190
Analyst Note:
This image shows an American F/A-18 fighter aircraft armed with two AGM-154 Joint Standoff Weapon (JSOW) air-delivered bombs taking off to conduct strikes against Houthi forces in Yemen. The F/A-18 likely has two more AGM-154-series munitions carried on the opposite side of the aircraft, for a total of four bombs. The JSOW has multiple variants which are fitted with different warheads, including a submunition payload (AGM-154A and AGM-154B models), BLU-111 500-pound bomb (AGM-154A-1), and a Bomb Royal Ordnance Augmented Charge (BROACH) multi-stage penetrator warhead (AGM-154C or AGM-154C-1). All variants are externally identical without markings, with the exception that the AGM-154C and C-1 have a small reflective window on the bottom of the nose for the terminal infrared (IR) seeker. The munitions in the image are most likely AGM-154A-1 or AGM-154C-series bombs, due to the lack of reported submunitions following the strikes. (ARES)
OSMP1207
Analyst Note:
This image shows an unexploded WDU-45/B, the second stage or penetrator warhead (also called a ‘follow-through’ warhead), of the Bomb Royal Ordnance Augmented Charge (BROACH) multi-stage warhead system used in the AGM-154C variant of the Joint Standoff Weapon (JSOW) air-delivered bomb. The first stage is a shaped-charge warhead designed help the second stage penetrate hardened targets before detonating. The Shadow/SCALP-EG missile also uses a multi-stage BROACH system, but with larger warheads. (ARES)
OSMP1196
Analyst Note:
This image shows an RGM-109-series Tomahawk Land Attack Missile (TLAM) being launched from the USS Curtis Wilbur (DDG 54), an Arleigh Burke-class guided missile destroyer. The RGM-/UGM-109 TLAM series are surface-to-surface cruise missiles fired from various platforms. The ‘R’ and ‘U’ in RGM and UGM, respectively, denote the intended launch platform, with ‘R’ denoting surface platforms, such as ships, and ‘U’ denoting subsurface platforms, such as submarines. (ARES)
OSMP1086
Analyst Note:
This image shows the section just forward of the Tamir missile’s forward fins and appears to incorporate the base of the active radar seeker (open end) and the laser proximity sensor part of the warhead fuzing system (mirrors/glass & opening in the casing). While the Tamir has been reported to physically impact some targets, the proximity fuze is designed to closely pass by the target, then detonate the high explosive fragmentation warhead thereby destroying the target. ‘Tamir’ is a Hebrew acronym for Til Meyaret, or ‘interceptor missile’. (ARES)
OSMP1081
Analyst Note:
Pictured is the Stunner’s dual electro-optical/infrared nose sensors which, while in flight, identify and avoid decoys; identify the target; and guides the kinetic warhead on the final phase of its journey into the target. The sensors are housed in the unique ‘dolphin head’-shape of the missile, featuring a clear tip. The electro-optical sensor acquires the target during daylight operations, while the infrared sensor acquires the target in low-light conditions. The ground-based Battle Management and Control (BMC) system identifies the target’s flight path, calculates the point of interception, and transmits this information to the Stunner by encrypted datalink. The missiles utilise a vertical launch system to allow for a complete 360° response area. (ARES)
OSMP1133
Analyst Note:
This image shows a relatively intact Shahed-131 one-way-attack (OWA) UAV with various components highlighted, including the GPS antenna array (light blue), fuselage (light purple), engine (yellow), wing stabiliser (orange), and nose cone (cyan, inside the red box). The nose cone attaches to the front of the fuselage and covers the warhead. (ARES)
OSMP875
Analyst Note:
This image shows a remnant of the aft motor section, which includes the venturi nozzle, of a North Korean KN-23/KN-24/Hwasong-11 series missile. The KN-23/KN-24/Hwasong-11 has a generally similar appearance to the Russian 9M7 ‘Iskander’ series of ballistic missiles, but has differences in performance and in some aspects of the construction. (ARES)