44 results
Analyst Note:
The internal components of large, complex munitions often feature markings to aid in assembly, supply chain oversight, and quality assurance. In this case, a data plate marked with the name of the manufacturer (“MBDA FRANCE”) has been affixed to one of the rear control fins (“EQ, VENTRAL, FIN TIP”) of the missile. The NATO Stock Number (NSN) is also visible. (ARES)
Analyst Note:
This image shows a Microturbo TRI 60-30 turbojet engine from a Storm Shadow-series air-launched cruise missile. Further remnants of the rear of the missile are also visible, including one of the rear control fins. The Storm Shadow has a range of more than 250 kilometres. (ARES)
Analyst Note:
The arming vane for a nose fuze (painted red) is visible on each of the two leftmost MAB-10B6 air-delivered bombs in this image. As the bomb falls, air passing over the arming vane causes it to spin, arming the fuze. (ARES)
Analyst Note:
The circles in this image indicate where the fixed fin assembly is connected to the bomb body. Fin assemblies such as this help stabilise the bomb as it falls, improving the predictability of the trajectory and thus precision. Fins also orient the bomb as it falls so that munition travels nose-down. Orientation of the bomb on impact can play a role in fuze functioning, as well as the distribution of explosive or other effects. (ARES)
Analyst Note:
The 9M22S is essentially the ‘full-sized’ version of the shorter 9M28S surface-to-surface rocket previously recorded in the OSMP. Both rockets carry the same 9N510 incendiary warhead, but differ in the length of their rocket motor sections, and thus range. (ARES)
Analyst Note:
The 9M28S surface-to-surface unguided rocket carries the 9N510 warhead, which disperses burning thermite-type incendiary elements over a wide area upon functioning. This munition is designed to start fires in target areas vulnerable to incendiary attack, including forests, ammunition dumps, and fuel storage sites. (ARES)
Analyst Note:
This image shows most of the forward half of a Tamir surface-to-air missile, including the guidance section and warhead, as fired by launchers in the Iron Dome system. These interceptor missiles are fast and manoeuvrable with a relatively small explosive payload. Their construction and low yield means that remnants are often recovered largely intact. (ARES)
Analyst Note:
This Iranian copy of the Chinese Type 63 107 mm rocket is marked with a red stripe and text to indicate it is of the high explosive incendiary (“H.E.I”) type. Markings also show that it was produced in 2007. (ARES)
Analyst Note:
Israeli illumination munitions—often finished in a distinctive yellow—are sometimes mistaken for high explosive munitions by observers more familiar with the NATO or U.S. marking systems. This image shows an M485-pattern illumination projectile, a base-eject type that uses a parachute-retarded canister containing a powerful candle to illuminate the battlefield.
Analyst Note:
The M825A1 155 mm smoke projectile makes use of white phosphorus (WP) to generate a brilliant white smoke. Whilst WP does have incendiary effects, the method of dispersal in the case of the M825A1 is optimised for screening and marking purposes. (ARES)
Analyst Note:
This image depicts an M117-series unguided aerial bomb. Belonging to a class of weapons referred to as ‘demolition bombs’—which use Tritonal or similar explosive compounds to generate a more powerful blast effect than TNT or Composition B—the M117 is an American design which dates to the Korean War era and is rarely seen in service with modern armed forces. (ARES)
Analyst Note:
The various Iranian Qaem-series guided air-delivered bombs can be difficult to differentiate from one another. In this case, the wing (forward fin) assembly distinguishes this Qaem-5 from the visually similar Qaem-1. Note also that the name 'Qaem' has applied by Iran to other, unrelated munitions. (ARES)
Analyst Note:
This component is one of four pneumatically controlled canards from the guidance section of a Paveway II precision guided munition (PGM) conversion kit. When a Paveway II conversion kit is fitted to a MK 82 series unguided air-delivered bomb (note markings), the munition receives a GBU-12 series designation. (ARES)
Analyst Note:
Like the more common 9M22S rocket, the 9M28S carries the 9N510 warhead, which dispenses 180 individual incendiary elements composed of a magnesium alloy shell filled with a thermite-like incendiary composition. (ARES)
Analyst Note:
These S-25-O air-to-surface rockets are each loaded into a single-barrelled O-25 rocket launcher (sometimes called a 'launch tube' or 'rocket pod') that is affixed to an aircraft hardpoint. The over-calibre high explosive fragmentation warhead (of 420 mm in diameter) protrudes from the front of the tube. (ARES)
Analyst Note:
The OF-NMR is a rocket-assisted mortar projectile, which uses a solid-fuel rocket motor located in the cylindrical portion of the body, below the ogive, to extend its range. Rocket-assisted mortar projectiles are rarely encountered. (ARES)
Analyst Note:
The 120 mm 3-Z-2 incendiary mortar projectile contains 6 incendiary elements, four large and two small. These are hollow steel ‘cups’ filled with an incendiary mixture of an unknown type, but understood to be comparable in effect to thermite. (ARES)
Analyst Note:
The AGM-88 High-Speed-Anti-Radiation-Missile (HARM) is an air-to-surface anti-radiation guided missile that seeks and destroys radar-based air-defence systems by detecting radar emissions, locking on to these, and using them to home in on a target. (ARES)
