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Delivered Munition
A munition that has been employed—e.g., fired, dropped, or launched—from a delivery platform. The munition may have either functioned or failed to function.
OSMP32
Analyst Note:
This 9M27K-series surface-to-surface cargo rocket is loaded with either 9N210 or 9N235 high explosive fragmentation (HE-FRAG) submunitions. These models are nearly identical in construction, differing primarily in the nature of the pre-formed fragments they carry. (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)
OSMP972
Analyst Note:
This image shows an aerosurface or ‘strake’ from a Joint Direct Attack Munition (JDAM) bomb guidance kit of the type fitted to MK 82-series 500-pound air-delivered bombs. The JDAM kits compatible with MK 82 bombs have aerosurfaces that are affixed near the nose of the bomb—rather than around the widest part of the bomb body, as seen in JDAM kits that are compatible with the larger MK 83 or MK 84 bombs. (ARES)
OSMP892
Analyst Note:
MK 84 unguided air-delivered bombs can be fitted with a variety of tail kits, or with guidance kits which convert them into precision guided munitions (PGMs). When an air-delivered bomb impacts a building or the ground without functioning, the tail or guidance kit may be sheared off. With these separated from the munition—and in the absence of other identifying features, such as a seeker fitted to the nose of the weapon—it becomes very difficult to determine whether the bomb was guided or unguided. (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)
OSMP963
Analyst Note:
This image shows an actuator from a Storm Shadow-series missile. Actuators are components of guided munitions that are most often used to move control surfaces (e.g., fins and wings), enabling the munition to adjust its course in-flight in response to guidance commands. In this case, the component is fitted with a ‘data plate’ that indicates it was manufactured by MBDA France. (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)
OSMP960
Analyst Note:
This image shows the rear of the second stage of the penetrator warhead (also called a ‘follow-through’ warhead) of the Bomb Royal Ordnance Augmented Charge (BROACH) multi-stage warhead system present in the Storm Shadow/SCALP-EG missile. The cylindrical object in the centre of the warhead (with a data plate marked “THALES”) is the fuze. (ARES)
OSMP967
Analyst Note:
This image shows the first stage of the Bomb Royal Ordnance Augmented Charge (BROACH) multi-stage warhead used by the Storm Shadow/SCALP-EG missile. The BROACH uses a shaped-charge warhead (seen here) as its first stage, to help penetrate hardened targets, whilst the second stage comprises a conventional high explosive penetrator warhead (also called a ‘follow-through’ warhead) (ARES).
OSMP979
Analyst Note:
The remnant at left in this image is the second stage, or penetrator warhead, of the Bomb Royal Ordnance Augmented Charge (BROACH) multi-stage warhead as used in the Storm Shadow/SCALP-EG air-launched cruise missile. In this case, it has failed to function as intended. (ARES)
OSMP958
Analyst Note:
This image shows part of a heavy-duty suspension lug associated with the Storm Shadow air-launched cruise missile. This is made clear from dot-peened markings which include “STORM SHADOW USE ONLY” and identifiers such as a NATO Stock Number (NSN). (ARES)
OSMP957
Analyst Note:
The munitions remnant on the left of this image is part of a suspension lug associated with the Storm Shadow air-launched cruise missile, which is used to attach the munition to an aircraft. This component is of heavy construction, and as such often survives the missile’s functioning intact. This photograph purports to show remnants recovered from a Storm Shadow missile that was fired by Ukrainian forces into Russian territory, but this claim cannot be verified from the image alone. (ARES)
OSMP942
Analyst Note:
This image shows a rocket motor section from an MGM-140 ATACMS series surface-to-surface ballistic missile. The warhead section of the MGM-140 series missiles separate from the rocket motor before functioning, resulting in the rocket motor often being found relatively intact near the target. The MGM-140 series missiles use the same rocket motor, preventing a positive identification of the variant based off the rocket motor alone, unless the variant markings are visible. (ARES)
OSMP928
Analyst Note:
This remnant of an MGM-140 Army Tactical Missile System (ATACMS) surface-to-surface ballistic missile is marked to indicate it is the MGM-140A variant, a cluster munition which carries 950 M74 multi-purpose submunitions. Submunitions of this type are sometimes referred to by the acronym ‘anti-personnel and anti‑materiel (APAM)’. Additional markings indicate a manufacturing date (“10/96”; October 1996), a serial number (“411240”), and other information. (ARES)
OSMP436
Analyst Note:
Almost all cluster munitions, including this example, expel their submunitions during flight. The submunitions are often held in an internal frame, such as that visible here, prior to being expelled. Depending on the munition, these internal frames may be diagnostic for identification. They usually do not carry a significant explosive payload in their own right, and therefore often withstand the functioning of the munition relatively intact. (ARES)
OSMP795
Analyst Note:
Honeycomb-like internal structures are often used in aerospace applications to provide rigidity with reduced weight, and are sometimes constructed using materials which reduce radar cross-section by absorbing or scattering electromagnetic waves. (ARES)
OSMP118
Analyst Note:
The 9M27K3 surface-to-surface rocket is fitted with the 9N128K3 cargo warhead (seen here). This warhead carries a payload of 312 PFM-1 or PFM-1S scatterable anti-personnel landmines. (ARES)
OSMP859
Analyst Note:
The arming vane for a nose fuze (painted red) is visible on each of the two leftmost MAB-10B6 air-delivered bombs in this image. As the bomb falls, air passing over the arming vane causes it to spin, arming the fuze. (ARES)
OSMP856
Analyst Note:
The circles in this image indicate where the fixed fin assembly is connected to the bomb body. Fin assemblies such as this help stabilise the bomb as it falls, improving the predictability of the trajectory and thus precision. Fins also orient the bomb as it falls so that munition travels nose-down. Orientation of the bomb on impact can play a role in fuze functioning, as well as the distribution of explosive or other effects. (ARES)
OSMP823
Analyst Note:
The Blue Sparrow is one of a series of three of air-launched missiles originally designed by Rafael as targets to test ballistic missile defence systems. Blue Sparrow missiles can be fitted with either inert or high explosive (HE) warheads. The recovery of Sparrow-series boosters following a reported Israeli strike on an Iranian air-defence system could suggest that a derivative variant of the Blue Sparrow missile was further developed for engaging surface targets. (ARES)
OSMP864
Analyst Note:
This image shows what is probably just the body of an Israeli 155 mm smoke artillery projectile. Israel predominantly uses two varieties of 155 mm smoke munition: the M825 white phosphorous (WP) series of munitions, and the M150 hexachloroethane/zinc mixture (HC) munition. These munitions are externally near-identical, save for their markings. In this case, the markings are insufficient to determine whether the image shows an M825-series WP munition or an M150 HC munition. (ARES)
OSMP70
Analyst Note:
The 9Н123К (9N123K) cargo warhead is delivered by a 9М79К (9M79K) series surface-to-surface guided missile. This cluster munition carries fifty 9Н24 (9N24) high explosive fragmentation (HE-FRAG) submunitions, and is launched from the 9К79 Tochka series of tactical ballistic missile launchers. (ARES)
OSMP68
Analyst Note:
A 9N24 submunition is visible to the left of the 9N123K warhead in this image. This high explosive fragmentation (HE-FRAG) submunition is marked to indicate it was produced in 1989 and filled with A-IX-2 explosive composition. (ARES)