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Rocket or Missile
Rockets and missiles are two closely related types of powered munitions which utilise an internal propulsion method, typically a rocket motor, to maintain their rate of travel after launch. Rockets and missiles are typically relatively long and thin—with lengths ranging from 50 centimetres to 6.5 metres. Rockets are unguided those fitted with guidance systems are usually referred to as missiles. Missiles sometimes use propulsion methods other than rocket motors, such as turbojets. The effective range of rockets varies from as little as one kilometre to more than 40 kilometres, while missiles typically have a longer range — some more than 250 kilometres.
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Analyst Note:
Based on design features and an estimation of the munition’s apparent size relative to the personnel handling it, this image appears to show a 122 mm surface-to-surface rocket fitted with a high explosive fragmentation (HE-FRAG) warhead, although the specific model and country of origin are unclear. In Sudan there have been reports of Russian, Chinese, and domestically produced (Taka-02) 122 mm rockets being used. (ARES)
Analyst Note:
The remnants shown in this image (and in linked OSMP entries) are reported by the Ukrainian government to be from the Russian ‘Oreshnik’ missile. Available information on this munition is very limited at the time of writing. It is reported that the Oreshnik can carry either a nuclear or conventional payload. The Oreshnik is likely capable of carrying up to 6 independently targetable reentry vehicles (MIRVs). It is unclear how many warheads can be carried in each re-entry vehicle. In the case of this strike, there is insufficient imagery to make a determination on which warhead/MIRV was used. (ARES)
Analyst Note:
This image shows the launch of an Iranian Paveh surface-to-surface cruise missile in Iraq. The munition was fired by Iranian proxy forces and reportedly targeting Israel. Some sources indicate the Paveh has been renamed the ‘Jamal-10’, whilst others claim it is being locally produced in Iraq by Iranian proxy forces. With an estimated 75% of the missile’s components coming from outside Iran, distributed production is certainly possible. The missile has two large wings located forward of the munition’s midpoint, three smaller fins towards the tail, and four actuated fins around the tail. The initial launch is accomplished with a solid-propellant rocket motor, which gives way to a turbo jet flight motor mounted on top of the missile, towards the tail. (ARES)
Analyst Note:
This image shows a screenshot from one of the videos released by the Kuwait Civil Aviation showing a one-way attack (OWA) unmanned aerial vehicle (UAV) striking the Kuwait International Airport. The munition’s distinctive delta-wing configuration and general size, shape, and manner of flight are consistent with the Shahed series of OWA UAVs. The related entry shows a Mado MD550 engine recovered following this strike, a model used to power the Shahed-136 series, enabling a more precise identification. (ARES)
Analyst Note:
This image shows an external portion of an Israeli Ra'am Eitan missile, a type of cluster munition fired from the Lahav (PULS) mobile rocket launcher. The yellow diamonds marked on the exterior of the munition are used to indicate a cluster munition. Other markings appear to indicate that this example was manufactured in 2017. (ARES)
Analyst Note:
The component pictured here is a small turbofan engine from a Tomahawk missile. Missiles are vertically launched from the Typhon Missile System (named for a monster of Greek mythology), which is also capable of launching the Standard SM-6 guided missile. The Tomahawk missile is ejected from its launch tube under gas pressure, then the solid propellant of the booster motor section (Mk 135 booster produced by L3Harris) propels the missile until the turbofan engine (F107-WR-402 for Block III/IV or F415 for Block IV/V, both produced by Williams International) in the propulsion section is initiated and the booster motor section drops away. The propulsion section also supports the four tail fins, which are released by the two-piece continuity shroud upon launch. (ARES)
Analyst Note:
This image shows an AGM-114R2 Hellfire II missile. The AGM-114R2 is an enhanced version of the the AGM-114R multi-role missile, which is designed to engage a wide variety of targets. The Hellfire R-series missile are equipped with a multi-purpose warhead that can engage armoured or unarmoured vehicles on land or sea, as well as personnel in the open or in buildings. Reports indicate that the AGM-114R2 features improvements to its guidance software and tracking to increase accuracy against moving targets, as well as incorporating an adjustable height-of-burst (HOB) capability which allows it to detonate at a pre-determined height above the ground. (ARES)
Analyst Note:
This image depicts what appears to be a WDU-42/B penetrator warhead as used in the AGM-158 JASSM series of missiles. The WDU-42/B is a 1,000-pound-class blast/fragmentation penetrator warhead designed to destroy hardened or reinforced targets. At the rear of the warhead, an FMU-156/B fuze is visible. This fuze is pre-programmed before launch according to the type of intended target. (ARES)
Analyst Note:
This munition, believed to be of Israeli origin, has been documented at a number of strike sites in Lebanon, Gaza, and Iran. Although distinctive remnants permit its tentative identification, the lack of a confirmed model name means this munition has been assigned a Temporary Munitions Identifier (TMID) by ARES. This appears in the Tentative Model field of the OSMP so that all records of this munition in the database can be linked under one temporary name. (ARES)
Analyst Note:
This image shows a Lancet-series one-way attack (OWA) UAV. It strongly resembles the Z-51E made by Zala Aerospace, a Russian manufacturer, although this cannot be confirmed from the available image. The Lancet series of drones can carry a variety of different warheads, including blast, fragmentation, thermobaric, and High Explosive Anti-Tank (HEAT). (ARES)
Analyst Note:
It is reported that this jet engine was recovered from the wreckage of a Geran-5 one-way attack (OWA) UAV. It is most likely a Telefly TF-TJ2000A model, manufactured by Telefly Telecommunications Company in China. It is reported that the TF-TJ2000A engine produces 200 kg of thrust; this is a significant increase in thrust compared to the Telefly JT80 engine used on the Shahed-238 (Geran-3) UAV, which produces approximately 80 kg of thrust. (ARES)
Analyst Note:
This image shows the remains of a Russian Geran-5 drone. These drones are reported to be roughly 6 meters long and have a wingspan of up to 5.5 meters. They are fitted with a warhead weighing approximately 90 kg and have a range of about 1,000 km. (ARES)
Analyst Note:
Considered with additional contextual materials, it is assessed that this image shows the rocket motor section from a 122 mm incendiary rocket, specifically the 9M22S or 9M28S models. Both rockets carry the same warhead, but use rocket motors of different lengths; not enough of this motor is visible to positively identify the model. (ARES)
Analyst Note:
This image shows a stepped component positioned at the front of the warheads carried by 122mm 9M22S and 9M28S incendiary rockets. This structure helps to push the ML-5 incendiary elements out of the rear of warhead once the fuze in the nose functions. It is a relatively distinctive component, and commonly found in the vicinity of where the incendiary elements fall. (ARES)
28 March 2026
