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 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)
The UMPK guidance package is a ‘bolt-on’ kit that can be fitted to unguided air-delivered bombs to convert them to guided munitions. The UMPK kit also greatly extends the range of the munition to which it is fitted, allowing aircraft to strike from beyond the range of many air-defence systems. Currently only Russia manufacturers and uses these kits. (ARES)
This image shows a Telefly JT80 jet engine, as used on Shahed-238 (Geran-3) UAVs. These jet engines are manufactured in China by Telefly Telecommunications Company. According to the manufacturer, each engine produces approximately 80kg of thrust. (ARES)
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)
The AGM-154 Joint Standoff Weapon (JSOW) is a guided air-delivered ‘glide bomb’ that allows for long-range strikes using an unpowered munition. The AGM-154C and AGM-154C-1 variants (a remnant of the latter pictured here) carry a Bomb Royal Ordnance Augmented Charge (BROACH) multi-stage warhead which uses a WDU-44 shaped-charge warhead as its first stage, to help penetrate hardened targets, whilst the WDU-45 second stage comprises a conventional high explosive penetrator warhead (also called a ‘follow-through’ warhead). The AGM-154C-1 is described by the U.S. Navy as their “first air-to-ground Network-Enabled Weapon (NEW) capable of attacking stationary land and moving maritime targets. It includes GPS/INS guidance, terminal IR seeker and a Link 16 weapon data link. Integration of the Link-16 weapon data link and updated seeker software algorithms provide a capability against at-sea moving/relocatable targets.” (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 depicts remnants from a M999 (‘Barak Eitan’) 155 mm cluster munition. Reports indicate that the M999 artillery projectile carries nine M99 Dual-Purpose Improved Conventional Munition (DPICM) submunitions. (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)
