The impact or effect the munition is intended to have
Functional use (10)
The specific model of munition pictured
Tentative Model (293)
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The external organisation that documented the munition
Research Organisation (6)
Colour of the munition pictured
Base Colour (12)
Colour of all, or some, of the markings on the munition
Marking Colour (11)
Language or script of the marking on a munition
Marking Script (10)
Condition of the munition pictured
Condition (6)
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.
The munition indicated is a one-way-attack (OWA) UAV fitted with a PG-7-series high explosive anti-tank (HEAT) warhead. Not enough of the warhead is visible to provide a positive ID on which model of PG-7-series projectile it was harvested from. (ARES)
This image appears to show a remnant from either a 9M38- or 9M317-series surface-to-air missile. Positive identification of this munition cannot be made based on the imagery in this source alone; a rear control fin is visible in image but the 9M38- and 9M317-series missiles use indistinguishable rear fins. (ARES)
This image appears to shows the remnants of either a 9M38- or 9M317-series missile, however positive identification of this surface-to-air missile cannot be made based solely on the imagery in this source. The 9M38- and 9M317-series missiles are close in design and function, and are predominantly fired from the Buk family of surface-to-air missile (SAM) systems. The Buk-M2E SAM system is known to be in service in Venezuela, having been delivered under a Russian contract beginning in 2015. The source video for this entry shows the destroyed remains of a Buk-M2E launch vehicle, known as the 9A316E. (ARES)
This image shows a WDU-36 series warhead as used in the RGM-/UGM-109 Tomahawk series of cruise missiles. The warhead design suggests this is likely a WDU-36/B from an RGM-/UGM-109E missile. The RGM-/UGM-109E Tomahawk Land Attack Missile (also known as TLAM Block IV) is an improved version of the BGM-109C TLAM-C. In cases where the missile strikes a building but does not function as intended, the dense, comparatively heavy warhead is often projected forwards of the point of impact. (ARES)
This image shows a WDU-36/B warhead as used in the RGM-/UGM-109 Tomahawk series of missiles. The WDU-36/B is the improved, lighter version of the previous WDU-25/B warhead. It is reported that the titanium-cased WDU-36/B weighs around 310 kg and carries a main charge of approximately 120 kg of PBXN-107 high explosives. (ARES)
This image shows a one-way-attack (‘sacrificial’) UAV with the apparent warhead broken off. It is believed to have been attached to the grey mechanism located at the rear of the UAV, likely separating when the UAV was downed. (ARES)
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)
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)
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)
This image shows a one-way attack (OWA) UAV fitted with a high explosive anti-tank (HEAT) warhead adapted from a PG-7 series recoilless gun projectile. (ARES)
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)
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)
This image shows a Hydra-70 rocket fitted with an Advanced Precision Kill Weapon System (APKWS) guidance kit, converting it into a guided missile. In this case, the missile features an M151 high explosive (HE) warhead fitted with either an M427 or M423 point-detonating (PD) fuze. The rocket motor model cannot be determined from this source alone, but it is most likely to be a MK 66-series motor. The launcher appears to be a LAND-LGR4 model produced by Arnold Defense. (ARES)
Positive identification of this surface-to-air missile cannot be made based on the imagery in the source. The items highlighted in this image are most likely the remains of either a 9M38- or 9M317-series missile, based on fin construction and their size relative to the individual posing in the foreground. These two missiles are close in design and function, and are predominantly fired from the Buk series of SAM systems. (ARES)
The 9N314M warhead shown here can be used in both 9M38- and 9M317-series missiles. In this particular case, according to the source, it was taken from a 9M38M1 missile. (ARES)
Although the source claims that this image shows a Buk-M3 surface-to-air missile system, this imagery is not sufficient to determine whether the remnants highlighted are from a 9M38-or 9M317-series guided missile. (ARES)
This guided munition is built around a sacrificial DJI Avata-series UAV that has been fitted with an improvised explosive device (IED). From front to back, it consists of an impact switch made from a syringe, the main charge (yellow/white material in a plastic bag), and a battery that acts as the power source. While crudely made, it is probably still functional. (ARES)
In this case, the tentative identification of this munition is possible based on an analysis of its silhouette, particularly the distinctive detachable warhead compartment that can be seen hanging from the base of the munition's body. In many cases, such an identification technique would not be possible to apply with confidence. (ARES)
This image represents the first documented instance of a Shahed-series UAV carrying an R-60 air-to-air missile. This appears to add a new capability to the Shahed, enabling it to target enemy aircraft. Arming UAVs to counter interception and engage alternative targets is an emergent trend. Previously, unmanned surface vessels (USVs) employed by the Ukrainian Armed Forces have been observed carrying R-73 air-to-air missiles, for example. (ARES)
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)
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)
This munition remnant is marked with a manufacturer’s CAGE Code (“MFR-05DN8”) which indicates it was produced by Klune Industries. Klune Industries is a sub-contractor on the GMLRS contract. (ARES)
This munition remnant is marked with a manufacturer’s CAGE Code (“MFR-62313”) which indicates it was produced by Lockheed Martin. Lockheed Martin is the primary contractor that makes GMLRS missiles. (ARES)
This image shows a remnant from an American M30 Guided Multiple Launch Rocket System(GMLRS) missile, which carries M77/M101 submunitions. The yellow diamond markings indicate a payload of explosive submunitions. (ARES)
This munition remnant is marked with a manufacturer’s CAGE Code (“MFR-57413”) which indicates it was produced by the Maine Machine Products Company, a sub-contractor on the GMLRS contract. (ARES)
This image shows several 107 mm rockets of the Type 63 pattern. Whilst developed by China, munitions of this design are now produced by several countries around the world, including Iran, North Korea, and Sudan. The state-owned Military Industry Corporation (MIC) of Sudan produces a copy of the Type 63 known as the TAKA-01, TAKA-1, or TAKA-107. (ARES)
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)
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)
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)
This image shows remnants of a Russian Kh-101 air-launched cruise missile. The remnant on the right is the rearmost tail section of the missile. (ARES)
This image shows a remnant of the TRDD-50A(M) (ТРДД-50А(M)) turbojet engine, which powers Kh-101 and Kh-59M missiles. Other models of Russian cruise missiles are known to use other variants of the TRDD-50. (ARES)
Two closely related types of powered munitions 
