1–100 of 681
Current Filter
Functioned Munition
The munition has either partially or fully operated and the intended effect has occurred. For explosive munitions, this usually means a detonation.
Analyst Note:
This image shows an external portion of an Israeli Ra'am Eitan missile, a type of cluster munition fired from the Lahav (PULS) mobile rocket launcher. The yellow diamonds marked on the exterior of the munition are used to indicate a cluster munition. Other markings appear to indicate that this example was manufactured in 2017. (ARES)
Analyst Note:
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)
Analyst Note:
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)
Analyst Note:
This image shows a stepped component positioned at the front of the warheads carried by 122mm 9M22S and 9M28S incendiary rockets. This structure helps to push the ML-5 incendiary elements out of the rear of warhead once the fuze in the nose functions. It is a relatively distinctive component, and commonly found in the vicinity of where the incendiary elements fall. (ARES)
Analyst Note:
This image shows a DC motor from a Tomahawk missile, manufactured by Globe Motors of Dayton, Ohio, in the United States (part # 471A118 and serial # 7250). Globe Motors was acquired by Allied Motion in August 2013, and has since been renamed Allied Motion at Dayton. This DC motor is used as an actuator to assist in steering the Tomahawk to its target based upon input from the aviation section in the forward body assembly. Such motors often survive detonation and can serve as diagnostic remnants. (ARES)
Analyst Note:
Components matching those seen here have been documented at other sites associated with the detonation of RGM-/UGM-109 Tomahawk cruise missiles. See, for example, OSMP 1199, 1218, 1191, 1193, and 1444. (ARES)
Analyst Note:
The munition remnant pictured here is marked with a Federal Stock Number (FSN; predecessor to the National Stock Number, or NSN, found on more modern munitions) that indicates it is part of a MIM-23B Improved HAWK surface-to-air missile. Other details, including the manufacturer (“Raytheon Company”), are also visible. The FSN was replaced by the NSN in 1974, indicating that this munition must have been manufactured before that time. This is consistent with the recorded U.S. export of the MIM-23B to Iran in 1972. (ARES)
Analyst Note:
This image shows remnants from a MIM-23 Homing All the Way Killer (HAWK) surface-to-air missile. U.S. government documents show that MIM-23B Improved HAWK systems were exported to Iran in 1972. Iran has since manufactured a reverse-engineered version of the system. (ARES)
Analyst Note:
This image shows the remains of the attitude control section of either a PAC-3 CRI or PAC-3 MSE missile. This section contains the attitude control motors, used in combination with control fins to guide and adjust the missiles on its way to the target. It is difficult to determine which of the two models this wreckage belongs to due the similarities of this section in both missiles and the absence of other distinctive components. (ARES)
Analyst Note:
This image shows the remnants of a PAC-3 Cost Reduction Initiative (CRI) missile. The PAC-3 family of missiles are hit-to-kill interceptors that defend against incoming ballistic missiles, cruise missiles, aircraft, and other targets primarily by using kinetic impact. However, it is important to note that these missiles contain a high explosive fragmentation (HE-FRAG) “lethality enhancer” warhead. These warheads are much smaller than what would normally be expected on a surface-to-air missile of this size, but still present a hazard if it fails to function as designed. (ARES)
Analyst Note:
The AGM-154 Joint Standoff Weapon (JSOW) is a guided air-delivered ‘glide bomb’ that allows for long-range strikes using an unpowered munition. The AGM-154C and AGM-154C-1 variants (a remnant of the latter pictured here) carry a Bomb Royal Ordnance Augmented Charge (BROACH) multi-stage warhead which uses a WDU-44 shaped-charge warhead as its first stage, to help penetrate hardened targets, whilst the WDU-45 second stage comprises a conventional high explosive penetrator warhead (also called a ‘follow-through’ warhead). The AGM-154C-1 is described by the U.S. Navy as their “first air-to-ground Network-Enabled Weapon (NEW) capable of attacking stationary land and moving maritime targets. It includes GPS/INS guidance, terminal IR seeker and a Link 16 weapon data link. Integration of the Link-16 weapon data link and updated seeker software algorithms provide a capability against at-sea moving/relocatable targets.” (ARES)
Analyst Note:
This image shows a Mk 104 Dual Thrust Rocket Motor (DTRM), the second-stage rocket motor for the SM-2, SM-3 Blk I, and SM-6 missiles. Based on the strakes or fins attached to this Mk 104, it can be determined that it was part of an SM-3 Blk I series missile. (ARES)
Analyst Note:
This image provides a close-up view of the bottom of the MK 136 Third Stage Rocket Motor section from a RIM-161 Standard Missile 3 (SM-3) Blk I guided missile. The integral warm gas/cold gas attitude control system, including its four venturis, is visible. (ARES)
Analyst Note:
This image shows the MK 136 Third Stage Rocket Motor of a U.S. RIM-161 Standard Missile 3 (SM-3) Blk I interceptor missile. The SM-3 Blk I variants share the same propulsion sections, but have differences in the kill vehicle section. The SM-3 Blk II variants are substantially different, including new, larger-diameter propulsion sections. SM-3 missiles have a booster, dual-thrust rocket motor, third-stage rocket motor, and an altitude control section in the kill vehicle. (ARES)
Analyst Note:
This image depicts remnants from a M999 (‘Barak Eitan’) 155 mm cluster munition. Reports indicate that the M999 artillery projectile carries nine M99 Dual-Purpose Improved Conventional Munition (DPICM) submunitions. (ARES)
Analyst Note:
This sheet-metal body component is marked with a manufacturer’s CAGE Code (“MFR-59518”) which indicates it was produced by GlenDee Corp. of Moorpark, California, which does business as Metalagraphics, Inc. (MGI). (ARES)
Analyst Note:
Moog Inc.—headquartered in East Aurora, New York, as marked on this munitions remnant—describes itself as a “worldwide designer, manufacturer, and integrator of precision control components and systems”. Moog supplies actuator and control components to the prime contractor on the Miniature Air-Launched Decoy (MALD) programme, Raytheon. (ARES)
Analyst Note:
This image shows the rear section of a Hydra-70 rocket. The Hydra-70 uses the MK 66 series of rocket motors, visible here, but can be fitted with at least 11 different warheads. They can also be fitted with the Advanced Precision Kill Weapon System (APKWS) ‘bolt-on’ guidance kit, converting an unguided rocket into a guided missile. From the available imagery, it is not clear with which warhead or guidance section this munition may have been fitted. (ARES)
Analyst Note:
This image shows the venturi and tailfin assembly from a 57 mm S-5 series rocket. The S-5 series of rockets are commonly used around the world in a variety of roles, including air-to-surface and surface-to-surface. Unfortunately, from this image alone the specific model and country of origin cannot be determined. (ARES)
Analyst Note:
Based on the tail-fin assembly design and relative size, the item pictured appears to be a 122 mm rocket. However, it is unclear if this image shows a Russian 9M22-series (‘Grad’) rocket, a Chinese Type 81 rocket, or a similar variant from a different country of origin. (ARES)
Analyst Note:
This images appears to show the remnants of a 122 mm rocket. It is unclear what the country of origin is, but it is most likely a 9M22-series or Type 81-series rocket. (ARES)
Analyst Note:
This image shows the damaged rocket motor section of a ballistic missile that was fired by the Houthis in Yemen towards Israel and likely intercepted. The Houthis employ ballistic missiles that are supplied by Iran, and given different names. In Houthi service, the Iranian Kheibar Shekan missile is known as the Hatem-2. (ARES)