201–300 of 806
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:
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)
Analyst Note:
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)
Analyst Note:
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)
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 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)
Analyst Note:
This Russian air-delivered cluster bomb is marked with a threatening message directed at the French people: «Français! Changer la politique du président dans le pays, sinon ces bombes vont changer le lieu d'atterrissage!» (“French people! Change the president’s policy in the country, otherwise these bombs will change their landing site!”). (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:
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)
Analyst Note:
The physical features of this munition indicate that it is most likely an Iranian 60 mm ‘high explosive, long-range’ (“H.E. L.R.”) mortar projectile fitted with an AZ111A2 impact fuze. However, positive identification cannot be made based on the source imagery. (ARES)
Analyst Note:
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)
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:
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)
Analyst Note:
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)
Analyst Note:
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)
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 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)
Analyst Note:
The image shows a one-way-attack (OWA) UAV that appears to have crashed, but failed to function. It consists of an FPV chassis, as well as some of the essential components required for flight and the explosive charge (purple container). The initiator and other parts relevant to both flight and the munition’s function are not visible. This appears to be craft-produced ‘sacrificial’ UAV. (ARES)
Analyst Note:
This photo shows some of the lithium-ion power banks found within a Gerbera UAV. These are used to power the onboard avionics, control surfaces, communications hardware, camera, and other components. The quantity and type of batteries fitted to the Gerbera will often vary based on the role for which the UAV has been configured—one-way attack (OWA; i.e., a ‘sacrificial’ munition), reconnaissance, signal relay, or decoy—and which specific hardware has been installed to effect this mission. (ARES)
Analyst Note:
This photo shows the fuel bladder of a Gerbera UAV, which still contains some fuel. It is likely that a bladder is used—rather than a rigid tank—to save on both weight and cost. Some variants of the Gerbera have been observed to be fitted with a second bladder in the forward section of the fuselage, serving to extend the UAV’s range. (ARES)
Analyst Note:
The DLE60 two-stroke petrol (gasoline) engine pictured here is the standard engine found on Gerbera UAVs. It is produced by the Chinese company Mile Haoxiang Technology Co., Ltd. and marketed specifically for use in UAVs. Although the Gerbera is manufactured in Russia, the engine and many other key components continue to be supplied from Chinese sources. (ARES)
Analyst Note:
This image shows a Controlled Reception Pattern Antennas (CRPA) unit installed on a Gerbera-series UAV. CRPAs are specialised antenna arrays that help protect GPS receivers from interference, spoofing, and jamming. This particular model, featuring four antennas, was first observed on the Shahed-136 UAV and has since been routinely seen fitted to Gerbera-series UAVs. An alternative array, with six antenna elements, has also been observed, reflecting the varied and ever-evolving state of electronic warfare in Ukraine. (ARES)
Analyst Note:
A Gerbera-series UAV is pictured here being carried by just two Ukrainian soldiers. This highlights the Gerbera’s lightweight design—the airframe is mostly constructed from Styrofoam and wood, which saves on both weight and cost. This particular example does not bear signs of significant damage, suggesting that it either malfunctioned or was brought down by EW and crashed. (ARES)
Analyst Note:
This image shows an A40 Pro camera, manufactured by the Chinese company Viewpro UAV and design specifically for use in UAVs. The black box to the right of the camera is the control box which manages video output, camera control, and power. The manufacturer claims this model has a 40× optical zoom, AI detection and tracking, and 3-axis gyro-stabilisation. The company further claims that it can customise the onboard AI recognition based on “target characteristics” provided by the client. Numerous Gerberas fitted with this model of camera are known to have been recovered by Ukrainian forces, although it is by no means the only camera model in use. (ARES)
Analyst Note:
This image shows the front and interior surfaces of a wireless communications module recovered from a downed Gerbera UAV. Although labelled as an HX-50 industrial wireless modem (compatible with WiFi and 5G/4G networks and designed for fixed locations), analysis by Ukrainian military sources indicates that this component is, in fact, an XK-F358 mesh-network module which offers significantly more capabilities. Manufactured and sold by Shenzhen Xingkai Technology Co., Ltd., these modules are designed for, amongst other things, use in robots and unmanned vehicles. Gerbera UAVs have been found operating on a wide variety of frequencies and networks, and this type of module is well-suited to this use. (ARES)
Analyst Note:
Pictured is a navigation/GPS module recovered from a downed Gerbera UAV. This particular model is used with the 4-antenna CRPA module seen in OSMP1648. The four RX ports on the bottom are normally directly connected to the CRPA (antenna) module, with other connections made to the UAV’s flight controller and power sources. Some Gerberas have been recovered with CRPA modules bearing a different number of antennas; different navigation modules have been observed on these. (ARES)
