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Reported Location (49)

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Classification groups of key explosive munitions used in conflicts

Munition Category (8)

The impact or effect the munition is intended to have

Functional use (10)

The specific model of munition pictured

Tentative Model (381)

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Colour of the munition pictured

Base Colour (12)

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

Marking Colour (11)

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Marking Script (9)

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Condition (6)

Key features defining the operation mechanisms of a projectile

Mechanical Feature (10)

Short metal pins or bolts for holding together two plates or pieces of metal.
Rivet Holes, Screws, Rivets
Whether a munition is guided or unguided

Guidance (2)

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

Weight Class (14)

501–600 of 791

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Rivet Holes, Screws, Rivets
Short metal pins or bolts for holding together two plates or pieces of metal. Such rivet holes, typically filled with rivets, are found on multiple types of munition.
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)
OSMP1125
Analyst Note:
These images show a damaged Serat-01 engine which powers the Shahed-131 drone after its rocket-assisted launch. The Serat-01 is a copy of the MDR 208 engine, and is noticeably smaller than the MD550 which powers the larger Shahed-136. (ARES)
OSMP1117
Analyst Note:
This image shows the BSF-50, one of several warheads developed by Russia for the Shahed-136/Geran-2 to replace the original Shahed-136 warhead designed by Iran. The BSF-50 is a high explosive warhead with a fragmentation effect. (ARES)
OSMP1126
Analyst Note:
Depicted here is the MD-550 motor of a Shahed-136/Geran-2. This image was presented by Ukrainian President Zelenskyy as a fragment of the drone that reportedly hit the Chernobyl Nuclear Power Plant’s New Safe Confinement shelter. (ARES)
OSMP1076
Analyst Note:
This image shows the functioned rocket motor of an Israeli Carpet rocket. The Carpet uses a fuel-air explosive (FAE) warhead which is designed to function mines and improvised explosive devices (IEDs), clearing a target area for the advance of friendly forces. These rockets are fired from the Carpet rocket launcher, which is loaded with up to 20 rockets and can be fitted to a variety of vehicles. (ARES)
OSMP1063
Analyst Note:
The Armement Air-Sol Modulaire (AASM; ‘Modular Air-to-Ground Armament’) family of French bolt-on guidance kits are fitted to air-delivered bombs of various sizes in a similar fashion to American JDAM kits. In some marketing materials, the acronym HAMMER is used, standing for ‘Highly Agile Modular Munition Extended Range’. This refers, in part, to the rocket boosters fitted to munitions in the family to extend their effective range. (ARES)
OSMP1062
Analyst Note:
In this photo, a Ukrainian Sukhoi Su-25 ground-attack aircraft from the 299th Tactical Aviation Brigade, with the bort number ‘Blue 28’, is seen carrying an AASM-250 guided air-delivered bomb under its left wing. Available imagery shows that the AASM-250 has also been fitted to Mikoyan MiG-29 fighter aircraft, and can likely be carried by the Sukhoi Su-27 as well. (ARES)
OSMP1056
Analyst Note:
This image shows the rear portions of two different two different Spike Non-Line-of-Sight (NLOS) missiles, which each include the control section and part of the rocket motor. The Spike NLOS has been in service with Israel since 1987, and is currently in its sixth generation, or iteration, which comprises an unknown number of variants. At least three different warhead configurations are reported: high explosive fragmentation (HE-FRAG), high explosive anti-tank (HEAT), and a ‘multipurpose’ or anti-structure variant with a penetrating blast and fragmentation warhead. (ARES)
OSMP1058
Analyst Note:
This image shows a MK 84 2,000-pound bomb that has had its fuze and baseplate removed in order to access the explosive filler. The fuze, fuze retaining ring, and baseplate can be seen on the white sheet. The explosive material used to fill the bomb has been removed, possibly to be repurposed in improvised explosive devices or craft-produced munitions. Unexploded ordnance is often ‘harvested’ for these purposes. (ARES)
OSMP1046
Analyst Note:
This image shows a wing fragment from a SPICE-1000 bomb guidance kit. While there are no remnants of the bomb body visible, it can be determined that a MK 83-series 1,000-pound bomb or similar was used, as MK-83 series bombs are paired with the SPICE-1000 bomb guidance kit to form a complete munition. (ARES)
OSMP1033
Analyst Note:
This image shows part of the SUU-66 dispenser (sometimes called a ‘shell’) that forms part of a CBU-105 D/B cluster bomb unit. In U.S. service, a ‘cluster bomb unit’ designation includes both the dispenser or shell, as well as the payload. The CBU-105 series of cluster munitions consists of CBU-97-series munitions that are modified with a WCMD (Wind Corrected Munitions Dispenser) guidance kit. Both CBU-97 and CBU-105 series munitions are made-up of an SUU-66 dispenser filled with 10 BLU-108 submunitions. Each BLU-108 submunition contains 4 ‘skeet’ warheads that are ejected mid-air and independently seek out targets using an infrared sensor. A single skeet weighs 7.5 lb (3.4 kg) and contains a copper explosively formed penetrator (EFP) for armour penetration that is surrounded by a fragmentation ring offering some anti-personnel effect. (ARES)
OSMP903
Analyst Note:
Whilst relatively little is known about Burmese air-delivered bombs from publicly available sources, researchers (including those at ARES and Myanmar Witness) have been collecting evidence based on munitions’ physical features and markings. Combined with information from confidential sources, this has allowed for the tentative identification of several models. (ARES)
OSMP920
Analyst Note:
The Stunner surface-to-air missile fired by the David’s Sling air defence system is a two-stage interceptor, meaning that the munition contains two separate rocket motors for launch and propulsion. The first stage, or launch motor, detaches from the munition after a short time, before the second stage, or flight motor, ignites. The second stage motor, visible here, was found relatively intact. (ARES)
OSMP984
Analyst Note:
This image shows part of the warhead section of an MGM-140 Army Tactical Missile System (ATACMS) series tactical ballistic missile. This is the top of the warhead section, where it connects to the guidance section. A data plate is visible, giving information about the manufacturer (“Lockheed Martin Vought Systems”) and identifying this specific part (“WARHEAD, GUIDED MISSILE. HIGH EXPLOSIVE”. (ARES)
OSMP975
Analyst Note:
This image shows an SUU-30H/B, an air-delivered dispenser which can be configured to carry different submunition payloads. These can include 217 BLU-61 A/B, 650 BLU-63/B, or 650 BLU-86/B or BLU-86 A/B. The munition can also carry inert payloads. The specific combination of payload and dispenser determines the ‘Cluster Bomb Unit’ (CBU) designation, with SUU-30H/B dispensers being paired with different payloads to form the CBU-58 and CBU-71 series. Contextual information suggests that this dispenser was part of a CBU-58/B cluster munition, but this cannot be established from an assessment of this image alone. (ARES)
OSMP965
Analyst Note:
The internal components of large, complex munitions often feature markings to aid in assembly, supply chain oversight, and quality assurance. In this case, a data plate marked with the name of the manufacturer (“MBDA FRANCE”) has been affixed to one of the rear control fins (“EQ, VENTRAL, FIN TIP”) of the missile. The NATO Stock Number (NSN) is also visible. (ARES)
OSMP964
Analyst Note:
This image shows a Microturbo TRI 60-30 turbojet engine from a Storm Shadow-series air-launched cruise missile. Further remnants of the rear of the missile are also visible, including one of the rear control fins. The Storm Shadow has a range of more than 250 kilometres. (ARES)