1–100 of 774
Current Filter
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.
Analyst Note:
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)
Analyst Note:
This image shows an AGM-114R2 Hellfire II missile. The AGM-114R2 is an enhanced version of the the AGM-114R multi-role missile, which is designed to engage a wide variety of targets. The Hellfire R-series missile are equipped with a multi-purpose warhead that can engage armoured or unarmoured vehicles on land or sea, as well as personnel in the open or in buildings. Reports indicate that the AGM-114R2 features improvements to its guidance software and tracking to increase accuracy against moving targets, as well as incorporating an adjustable height-of-burst (HOB) capability which allows it to detonate at a pre-determined height above the ground. (ARES)
Analyst Note:
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)
Analyst Note:
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)
Analyst Note:
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)
Analyst Note:
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)
Analyst Note:
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)
Analyst Note:
3OF39 Krasnopol rounds are shipped in two parts as seen in this image. They are then assembled prior to employment. (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 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:
This image is a composite assembled from several screen captures taken from an IDF video. Due to camera movement and other factors, there may be some minor misalignment. (ARES)
Analyst Note:
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)
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)
