Where the munition is launched from and what it targets
Domain (7)
The type of fins visible on the munition
Fins Characteristic (5)
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.
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.
This image shows a fragment of the “inner petal assembly” of a Terminal High Altitude Area Defense (THAAD) system’s ‘Talon’ interceptor missile. The part number for the assembly (“23917ASSY1A62803-101 REV.E / E”), Commercial and Government Entity (CAGE) code (“07554”), manufacturer abbreviation (“CTL”), and serial number (“S/N DDLKD”) are visible. This CAGE code and manufacturer abbreviation are associated with CTL Aerospace Inc, a subcontractor for Lockheed Martin, the manufacturer of the THAAD system. It is not uncommon for complex munitions to be made by several different manufacturers, and thus multiple CAGE codes may be present as a result of the various subcontractors. (ARES)
This image shows a Mikholit glide bomb, with its warhead removed (green cylinder on the left side of the box). The fins that spring outward when deploye have been taped down. This Mikholit was reportedly recovered by the Israeli Defense Forces (IDF) from Hamas, who had captured the bomb after it failed to function when originally deployed by the IDF. (ARES)
This image shows two Mikholit air-delivered bombs (‘glide bombs’), and four Mikholit warheads. There are at least two different variants of warheads available for the Mikholit glide bomb. The green cylinder on the left is a blast (high explosive) warhead, whilst the other three warheads are shaped charge warheads which incorporate additional fragmentation. Blast warheads of this type have also been seen with red markings, while the shaped charge warheads have been seen with yellow markings. (ARES)
This image shows various remnants from GBU-39 air-delivered bombs, including two fuze wells. Each GBU-39 has only a single fuze well, indicating that this picture shows the remnants of at least two different GBU-39 bombs. (ARES)
This image and the related entries show fragments of an AGM-84 Standoff Land Attack Missile-Expanded Response (SLAM-ER) series missile. AGM-84 SLAM-ER missiles are AGM-84E Standoff Land Attack Missiles (SLAM) that incorporate certain upgrades, including wings to increase the missile's range. The AGM-84 series include the anti-ship ‘Harpoon’ variants, from which the SLAM and SLAM-ER series are derived. As a result, many remnants will be similar or identical between variants. The wing remnant here is diagnostic, however. (ARES)
This image shows the rear fin section that is attached to a M-302/Khaibar-1/Fadi series rockets to add guidance capabilities. This rear fin section is installed, along with a forward control section between the warhead and the rocket motor. The guided munition, now classified as a missile, is referred to as a Nasr-1/Nasr-2. A similar, but larger, rear fin section is fitted to Zelzal rockets to convert them to guided munitions. (ARES).
This image shows several GBU-53/B bombs photographed from above while on a munitions transport cart. GBU-53/B bombs are transported and loaded onto the aircraft with the wing assembly on the bottom. When the GBU-53/B is released from the aircraft, the bomb rotates, with the wing assembly side orienting as the top as the bomb glides to its target. (ARES)
This image shows the rocket motor of a Kheibar Shekan or Fattah-1 medium-range ballistic missile (MRBM). The Fattah-1 was publicly unveiled by Iran in June 2023, with very few images surfacing since that time. Due to the lack of available reference material, differentially identifying the Kheibar Shekan and Fattah-1 is difficult. The missile components displayed at unveilings and public displays are also often different from those used in production models. (ARES).
This image shows the copper cone of the shaped charge located at the front of the warhead fitted to a Shahed-131. The Ukrainian armed forces have recorded that the cone measures 111 mm in diameter and 162 mm in depth. The warhead is lined with cubic pre-formed fragments of 7 mm in diameter. The explosive content of the warhead is estimated to be between 10 and 15 kg. (ARES)
This image shows two MAM-L guided air-delivered bombs affixed to the wing of a Bayraktar TB2 drone. The MAM-L and TB2 are both produced in Türkiye by Roketsan and Baykar respectively. The MAM-L can have one of three different warheads: blast fragmentation, anti-tank, or thermobaric. The warhead section of each MAM-L in this image has “YIPE/BF” visible. ‘YIPE’ is the abbreviation of the warhead type in Turkish: Yüksek Infilaklı Parçacık Etkili (‘high explosive fragmentation’, in English). The ‘BF’ also indicates that these MAM-L munitions are of the blast-fragmentation variant. The warhead of a MAM-L cannot be determined from an external assessment without viewing markings such as these (or a clear view of the data plate, which can be seen on the aft portion of the MAM-L). (ARES)
This image shows several remnants of a MAM-L bomb that are typically found after functioning. The actuated fins, as well as the fixed fins, are visible, along with various components of the control section that actuate the fins. The actuated fins attach to the control section, at the rear of the bomb, while the fixed fins attach to the middle of the bomb body. (ARES)
This image shows the section just forward of the Tamir missile’s forward fins and appears to incorporate the base of the active radar seeker (open end) and the laser proximity sensor part of the warhead fuzing system (mirrors/glass & opening in the casing). While the Tamir has been reported to physically impact some targets, the proximity fuze is designed to closely pass by the target, then detonate the high explosive fragmentation warhead thereby destroying the target. ‘Tamir’ is a Hebrew acronym for Til Meyaret, or ‘interceptor missile’. (ARES)
Pictured is the Stunner’s dual electro-optical/infrared nose sensors which, while in flight, identify and avoid decoys; identify the target; and guides the kinetic warhead on the final phase of its journey into the target. The sensors are housed in the unique ‘dolphin head’-shape of the missile, featuring a clear tip. The electro-optical sensor acquires the target during daylight operations, while the infrared sensor acquires the target in low-light conditions. The ground-based Battle Management and Control (BMC) system identifies the target’s flight path, calculates the point of interception, and transmits this information to the Stunner by encrypted datalink. The missiles utilise a vertical launch system to allow for a complete 360° response area. (ARES)
This image shows a relatively intact Shahed-131 one-way-attack (OWA) UAV with various components highlighted, including the GPS antenna array (light blue), fuselage (light purple), engine (yellow), wing stabiliser (orange), and nose cone (cyan, inside the red box). The nose cone attaches to the front of the fuselage and covers the warhead. (ARES)
This image shows a remnant of the aft motor section, which includes the venturi nozzle, of a North Korean KN-23/KN-24/Hwasong-11 series missile. The KN-23/KN-24/Hwasong-11 has a generally similar appearance to the Russian 9M7 ‘Iskander’ series of ballistic missiles, but has differences in performance and in some aspects of the construction. (ARES)
