Key features defining the operation mechanisms of a projectile
Mechanical Feature (10)
Whether a munition is guided or unguided
Guidance (2)
Where the munition is launched from and what it targets
Domain (7)
The type of fins visible on the munition
Fins Characteristic (6)
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.
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)
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)
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)
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)
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)
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)
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)
The component shown in this image is a GPS antenna for the AGM-158 Joint Air-to-Surface Standoff Missile (JASSM). It is marked to indicate its manufacturer (“Ball Aerospace & Technologies Corp.”; now operating as BAE Systems’ Space & Mission Systems division) and with other key information, including a part number and contract number. (ARES)
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)
This image shows an unexploded Iranian submunition of unknown designation. Visually similar examples have been documented following Iranian ballistic missile strikes on Israel in June 2025 and March 2026. At least two variants are believed to exist, but publicly available details remain limited at time of review. (ARES)
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)
This image shows a Low-Cost Unmanned Combat Attack System (LUCAS). The LUCAS one-way attack UAV is a U.S.-made, cost-effective ‘kamikaze drone’. LUCAS munitions can connect to one another via a mesh network, allowing multiple LUCAS drones to communicate in flight. The white square object connected to the munition by a cable appears to be a Starlink antenna, consistent with reported communication capabilities. Elon Musk has claimed that LUCAS operates only via Starshield, a Starlink-derived satellite network intended for government use. (ARES)
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)
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)
