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Classification groups of key explosive munitions used in conflicts

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Grey / Silver
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Calibre (77)

Weight class of the aerial bomb pictured

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101–200 of 1,250
OSMP1752
Analyst Note 2 March 2026
Based on design features and an estimation of the munition’s apparent size relative to the personnel handling it, this image appears to show a 122 mm surface-to-surface rocket fitted with a high explosive fragmentation (HE-FRAG) warhead, although the specific model and country of origin are unclear. In Sudan there have been reports of Russian, Chinese, and domestically produced (Taka-02) 122 mm rockets being used. (ARES)
OSMP2284
Analyst Note 15 August 2026
This image shows a U.S. Area Denial Artillery Munition (ADAM), an anti-personnel scatterable landmine which is dispensed from the rear of M692 and M731 155 mm artillery gun projectiles. Each projectile contains 36 ADAM submunitions. The submunition can deploy up to seven tripwires out to 20 ft (6.1 m). Any movement of a tripwire or movement of the ADAM body will result in a small kill mechanism being ejected to a height of a 6–8 ft (1.8 m–2.4 m) prior to detonating. Each munition contains a small amount of depleted uranium. The ADAM was previously designated as either the M67 or M72, with the only difference being the self-destruct time delay. (ARES)
OSMP1896
Analyst Note 2 March 2026
The remnants shown in this image (and in linked OSMP entries) are reported by the Ukrainian government to be from the Russian ‘Oreshnik’ missile. Available information on this munition is very limited at the time of writing. It is reported that the Oreshnik can carry either a nuclear or conventional payload. The Oreshnik is likely capable of carrying up to 6 independently targetable reentry vehicles (MIRVs). It is unclear how many warheads can be carried in each re-entry vehicle. In the case of this strike, there is insufficient imagery to make a determination on which warhead/MIRV was used. (ARES)
OSMP1912
Analyst Note 2 March 2026
The tank visible in the background of the image appears to be a Chinese VT-4 (MBT-3000) model. The VT-4 is manufactured by Norinco and is intended primarily for export. (ARES)
OSMP2186
Analyst Note 10 June 2026
This image shows the launch of an Iranian Paveh surface-to-surface cruise missile in Iraq. The munition was fired by Iranian proxy forces and reportedly targeting Israel. Some sources indicate the Paveh has been renamed the ‘Jamal-10’, whilst others claim it is being locally produced in Iraq by Iranian proxy forces. With an estimated 75% of the missile’s components coming from outside Iran, distributed production is certainly possible. The missile has two large wings located forward of the munition’s midpoint, three smaller fins towards the tail, and four actuated fins around the tail. The initial launch is accomplished with a solid-propellant rocket motor, which gives way to a turbo jet flight motor mounted on top of the missile, towards the tail. (ARES)
OSMP2145
Analyst Note 10 June 2026
Highlighted are four GBU-31 Joint Direct Attack Munitions (JDAM) guided air-delivered bombs loaded onto the belly of a U.S. F-15E Strike Eagle aircraft. The GBU-31-series consists of a 2,000-pound-class bomb (Mk 84, BLU-109, or BLU-109A/B) and a guidance kit comprising a tail unit with four articulating fins and a guidance control unit with inertial navigation system (INS) and global positioning system (GPS) functions. The GBU-31 munitions seen here are built around the BLU-109, a penetrator munition with a solid nose and a thicker, one-piece body which flares slightly at the base. It has no body welds; the heavy steel base plate is held in place by an equally robust threaded steel closure ring. The BLU-109 is painted olive drab with a single yellow band towards the nose. (ARES)
OSMP2257
Analyst Note 27 April 2026
The component pictured here is a small turbofan engine from a Tomahawk missile. Missiles are vertically launched from the Typhon Missile System (named for a monster of Greek mythology), which is also capable of launching the Standard SM-6 guided missile. The Tomahawk missile is ejected from its launch tube under gas pressure, then the solid propellant of the booster motor section (Mk 135 booster produced by L3Harris) propels the missile until the turbofan engine (F107-WR-402 for Block III/IV or F415 for Block IV/V, both produced by Williams International) in the propulsion section is initiated and the booster motor section drops away. The propulsion section also supports the four tail fins, which are released by the two-piece continuity shroud upon launch. (ARES)
OSMP2276
Analyst Note 24 August 2026
Highlighted is a Russian POM-2 scatterable, high explosive, anti-personnel submunition which deploys six legs for stabilization upon impact and four pressure- and pull-sensitive 9.5m (31.17’) long tripwires which end in a ‘Y’ fashion with plastic weights. Upon deployment, nylon ribbons (seen in the foreground) are deployed to help ensure the submunition lands upright, in addition to the stabilizing legs. Originally designed to be dispensed by rockets and helicopters, the war in Ukraine has seen the POM-2 modified for deployment via drone, hand and even from RPGs. (ARES)
OSMP2275
Analyst Note 24 August 2026
Pictured is a Russian PFM-1 or PFM-1S submunition which are small plastic (low density polythene), liquid high explosive, anti-personnel scatterable landmines with a pressure fuze and may be green, white, sand or brown (shown) in color. The only difference between the models is that the PFM-1S incorporates a nominal self-destruct of 40 hours, though they may remain active for far longer and are known to randomly self-destruct for weeks after deployment. They weigh approximately 70 grams (2.47 oz.) and are typically dispensed from cannisters, but the war in Ukraine has seen them dispensed from drones as well. (ARES)
OSMP2155
Analyst Note 21 April 2026
This image depicts what appears to be a WDU-42/B penetrator warhead as used in the AGM-158 JASSM series of missiles. The WDU-42/B is a 1,000-pound-class blast/fragmentation penetrator warhead designed to destroy hardened or reinforced targets. At the rear of the warhead, an FMU-156/B fuze is visible. This fuze is pre-programmed before launch according to the type of intended target. (ARES)
OSMP2184
Analyst Note 28 April 2026
This munition, believed to be of Israeli origin, has been documented at a number of strike sites in Lebanon, Gaza, and Iran. Although distinctive remnants permit its tentative identification, the lack of a confirmed model name means this munition has been assigned a Temporary Munitions Identifier (TMID) by ARES. This appears in the Tentative Model field of the OSMP so that all records of this munition in the database can be linked under one temporary name. (ARES)
OSMP1839
Analyst Note 2 March 2026
Positive identification of the model of air-delivered bomb to which the UMPK kit is fitted cannot be made from the source imagery. Based on the size of the UMPK and historical use in the area, it is likely an OFAB-250-270 model. (ARES)
OSMP1894
Analyst Note 2 March 2026
It is reported that this jet engine was recovered from the wreckage of a Geran-5 one-way attack (OWA) UAV. It is most likely a Telefly TF-TJ2000A model, manufactured by Telefly Telecommunications Company in China. It is reported that the TF-TJ2000A engine produces 200 kg of thrust; this is a significant increase in thrust compared to the Telefly JT80 engine used on the Shahed-238 (Geran-3) UAV, which produces approximately 80 kg of thrust. (ARES)
OSMP1890
Analyst Note 2 March 2026
This image shows the remains of a Russian Geran-5 drone. These drones are reported to be roughly 6 meters long and have a wingspan of up to 5.5 meters. They are fitted with a warhead weighing approximately 90 kg and have a range of about 1,000 km. (ARES)
OSMP1851
Analyst Note 2 March 2026
The 3OF39 Krasnopol is a laser-guided, rocket-assisted 152 mm tank gun projectile carrying a high explosive fragmentation (HE-FRAG) warhead. The round is built and shipped with a cover over the optical sensor. This protective cover is fitted with a T-90 mechanical time delay fuze. Once fired, the T-90 fuze will initiate after a pre-selected time and will jettison the protective cover, exposing the optical sensor in the nose. The internal impact fuze, which can be set for immediate or delayed initiation, is then responsible for detonating the projectile. (ARES)
OSMP1837
Analyst Note 2 March 2026
Considered with additional contextual materials, it is assessed that this image shows the rocket motor section from a 122 mm incendiary rocket, specifically the 9M22S or 9M28S models. Both rockets carry the same warhead, but use rocket motors of different lengths; not enough of this motor is visible to positively identify the model. (ARES)