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Reported Location (51)

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Classification groups of key explosive munitions used in conflicts

Munition Category (8)

Emplaced munitions either activated remotely or by the target or victim.
Mine
Two closely related types of powered munitions
Rocket or Missile
The impact or effect the munition is intended to have

Functional use (10)

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Tentative Model (338)

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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 (9)

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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.

Calibre (75)

Weight class of the aerial bomb pictured

Weight Class (14)

801–900 of 1,090

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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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Current Filter

Mine
Emplaced munitions either activated remotely or by the target or victim.
OSMP871
Analyst Note:
This Blue Sparrow-series air-launched ballistic missile is being carried by an F-15C fighter aircraft from 106 Squadron Israeli Air Force. The missile is marked with the logos of three organisations involved in its development—the U.S. Missile Defense Agency, the Directorate of Defence Research & Development, and the Israel Missile Defense Organization—and the Blue Sparrow programme logo of the manufacturer (Rafael Advanced Defense Systems). The booster section also features bright-orange fins and markings consistent with its use as a target missile, here modified to accept a high explosive warhead. (ARES)
OSMP823
Analyst Note:
The Blue Sparrow is one of a series of three of air-launched missiles originally designed by Rafael as targets to test ballistic missile defence systems. Blue Sparrow missiles can be fitted with either inert or high explosive (HE) warheads. The recovery of Sparrow-series boosters following a reported Israeli strike on an Iranian air-defence system could suggest that a derivative variant of the Blue Sparrow missile was further developed for engaging surface targets. (ARES)
OSMP88
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)
OSMP70
Analyst Note:
The 9Н123К (9N123K) cargo warhead is delivered by a 9М79К (9M79K) series surface-to-surface guided missile. This cluster munition carries fifty 9Н24 (9N24) high explosive fragmentation (HE-FRAG) submunitions, and is launched from the 9К79 Tochka series of tactical ballistic missile launchers. (ARES)
OSMP68
Analyst Note:
A 9N24 submunition is visible to the left of the 9N123K warhead in this image. This high explosive fragmentation (HE-FRAG) submunition is marked to indicate it was produced in 1989 and filled with A-IX-2 explosive composition. (ARES)
OSMP828
Analyst Note:
The Stunner missile is the surface-to-air interceptor missile fired by the David’s Sling weapon system to defeat short-range ballistic missiles, cruise missiles, drones, and rockets. The Stunner does not carry an explosive warhead, instead relying on kinetic impact (also called the ‘hit-to-kill’ principle) to intercept ballistic missiles and other targets. (ARES)
OSMP87
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)
OSMP827
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)
OSMP12
Analyst Note:
This 9M27K-series surface-to-surface cargo rocket is carrying a payload of 9N210 or 9N235 high explosive fragmentation (HE-FRAG) submunitions. These submunitions are difficult to distinguish unless their external markings are visible, or a close examination is made. (ARES)
OSMP590
Analyst Note:
The MGM-140 Army Tactical Missile System (ATACMS) series includes variants with a variety of different payloads, including submunitions and unitary high explosive (HE) warheads. The number of submunitions carried and effective ranges also vary. Ukraine has reportedly received the MGM-140A and MGM-140B variants, which are externally visually identical and must usually be distinguished by markings. The MGM-140A carries 950 M74 submunitions, with an effective range of 165 km, while the MGM-140B carries only 300 M74 submunitions but has a longer effective range of 300 km. (ARES)
OSMP614
Analyst Note:
The crude launch arrangement depicted in this photograph shows the ease with which many simple rocket designs can be launched. Weapons such as this are used where precision fire is not a requirement; i.e., where the target might be a whole compound, neighbourhood, or settlement, rather than a specific building or vehicle. (ARES)
OSMP722
Analyst Note:
The 9M14 Malyutka anti-tank guided missile was designed and fielded by the Soviet Union in the 1960s. It uses an outdated guidance principle known as manual command to line-of-sight (MCLOS), in which the operator must manually adjust the course of the missile in flight. Nonetheless, this munition has been seen in several 21st-century conflicts. (ARES)
OSMP731
Analyst Note:
This image shows the nosecone from an Israeli Tamir surface-to-air missile. This component is often found as a remnant after the functioning of the missile. (ARES)
OSMP739
Analyst Note:
The AGM-179 Joint Air-to-Ground Missile (JAGM) is derived from the AGM-114 Hellfire series of air-to-surface missiles—and thus shares physical characteristics in terms of general construction, including rear fin placement. The marked weight of 52.0 kg (115 lbs) is generally believed to be an indicator that the rocket motor is from a JAGM; however, remnants marked with this weight have been observed from several years before the JAGM was initially fielded. (ARES)
OSMP727
Analyst Note:
In this image, four AGM-114 Hellfire-series missiles can be seen fitted to an M299-series missile launcher, itself attached to the stub wings of this Israeli AH-64 Apache helicopter. In theory, the Apache could be armed with up to sixteen Hellfire missiles, but fewer are carried in practice to allow for other weapons and sensor payloads (ARES).
OSMP711
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)
OSMP685
Analyst Note:
The Tamir Interceptor is the missile fired from Israel’s Iron Dome defence system to intercept incoming rockets, missiles, projectiles, and unmanned aerial vehicles (‘drones’). The Tamir uses a warhead with a relatively small explosive yield, which typically results in the guidance section, nosecone, and (spent) rocket motor falling to the ground relatively intact after functioning. (ARES)