Do not approach munitions
under any circumstances
Country or territory where the image was reported

Reported Location (48)

Year the image is reported to have been taken

Year (20)

Classification groups of key explosive munitions used in conflicts

Munition Category (8)

Two closely related types of powered munitions
Rocket or Missile
The impact or effect the munition is intended to have

Functional use (10)

The specific model of munition pictured

Tentative Model (364)

Search

The external organisation that documented the munition

Research Organisation (6)

Colour of the munition pictured

Base Colour (12)

Colour of all, or some, of the markings on the munition

Marking Colour (10)

Language or script of the marking on a munition

Marking Script (9)

Condition of the munition pictured

Condition (6)

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 (5)

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 (72)

Weight class of the aerial bomb pictured

Weight Class (14)

401–500 of 1,016

Current Filter

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.
Read more
OSMP1462
Analyst Note:
This image shows a remnant of the control section of the Arrow 2 ‘kill vehicle’, including the control fins. The blast-fragmentation warhead is located in the front section of the kill vehicle, forward of the control section, and is absent here due to the functioned state of the munition. (ARES)
OSMP1504
Analyst Note:
This image shows the rocket motor of an AGM-114 "Hellfire" series guided missile found in Jordan during the 12 day conflict between Israel and Iran. This specific Hellfire missile is likely an air-to-air "C-UAS" variant used to intercept one-way attack drones, such as those launched by Iran towards Israel, rather than the more common air-to-surface Hellfire missile variants. (ARES)
OSMP1412
Analyst Note:
This image shows a improvised rocket-assisted munition (IRAM). This particular munition consists of a 107 mm rocket motor with an industrial gas cylinder fitted in place of the standard warhead. The frost present on the cylinder indicates a pressurised gas was released. The yellow–green residue is consistent with a payload of chlorine gas. (ARES)
OSMP1227
Analyst Note:
The source for this entry reports that these remnants were left behind after the missiles were “recycled“. Explosive remnants of war (ERW) are often recycled for the value of their scrap metal, or ‘harvested’ by militant groups for the explosive material. These recycling attempts may result in the ERW exploding, potentially killing or injuring people. (ARES)
OSMP1401
Analyst Note:
The munition in this image has been integrated into a commercial off-the-shelf (COTS) small UAV. This UAV (‘drone’) adds powered and guided delivery and converts the munition into a guided missile—regardless of the original, intended delivery method. (ARES)
OSMP1403
Analyst Note:
The warhead of the OWA UAV indicated in this image cannot be positively identified from this photograph alone. It appears to be the warhead section of either an OG-9 series or OG-15 series high explosive fragmentation (HE-FRAG) projectile, with a GO-2 or similar impact fuze fitted in the nose. (ARES)
OSMP1366
Analyst Note:
This image shows an AR731-4000 Wankel-type engine produced by UAV Engines Ltd. of the United Kingdom, used in an Israeli Harop munition. Variants of the Harop used in the 2020 Nagorno-Karabakh War featured a similar Wankel engine, but were marked to indicate a different manufacturer and model name: “MBT ENGINE” and “H2251-5100-503”, respectively. (ARES)
OSMP1354
Analyst Note:
This image shows the remnants of a SkyStriker one-way attack UAV, manufactured by Elbit Systems of Israel. The SkyStriker can be fitted with various warhead options, including dual-purpose warheads weighing 5 or 10 kilograms. While it appears that a reconstruction was attempted with the remnants, the placement of the various components does not accurately represent an intact SkyStriker. (ARES)
OSMP1246
Analyst Note:
This image shows the flare from a Terminal High Altitude Area Defense (THAAD) system's ‘Talon’ kinetic interceptor missile. The flare is located at the aft end of the missile's booster engine. The ‘petals’ of the flare are initially flush, and are actuated into the deployed position, seen here, as part of the missile‘s functioning. (ARES)
OSMP1238
Analyst Note:
This image shows a fragment of the “inner petal assembly” of a Terminal High Altitude Area Defense (THAAD) system’s ‘Talon’ interceptor missile. The part number for the assembly (“23917ASSY1A62803-101 REV.E / E”), Commercial and Government Entity (CAGE) code (“07554”), manufacturer abbreviation (“CTL”), and serial number (“S/N DDLKD”) are visible. This CAGE code and manufacturer abbreviation are associated with CTL Aerospace Inc, a subcontractor for Lockheed Martin, the manufacturer of the THAAD system. It is not uncommon for complex munitions to be made by several different manufacturers, and thus multiple CAGE codes may be present as a result of the various subcontractors. (ARES)
OSMP1121
Analyst Note:
This image shows three different warheads developed by Russia for the Shahed-136/Geran-2 one-way attack (OWA) unmanned aerial vehicle (UAV), each of which differ from the original warhead designed by Iran for the Shahed-136. Left: A thermobaric explosive warhead; Middle: TBBCh-50M, a thermobaric explosive warhead; Right: OFZBCh-50, a high explosive warhead with an incendiary effect. Each of these warheads is also fitted with a fragmentation liner to increase the fragmentation effect generated when the warhead detonates. Some of the fragmentation liners may contain zirconium, a metal which is ignited when the warhead detonates, providing an additional incendiary effect. (ARES)
OSMP1302
Analyst Note:
This image and the related entries show fragments of an AGM-84 Standoff Land Attack Missile-Expanded Response (SLAM-ER) series missile. AGM-84 SLAM-ER missiles are AGM-84E Standoff Land Attack Missiles (SLAM) that incorporate certain upgrades, including wings to increase the missile's range. The AGM-84 series include the anti-ship ‘Harpoon’ variants, from which the SLAM and SLAM-ER series are derived. As a result, many remnants will be similar or identical between variants. The wing remnant here is diagnostic, however. (ARES)
OSMP832
Analyst Note:
This image shows the rear fin section that is attached to a M-302/Khaibar-1/Fadi series rockets to add guidance capabilities. This rear fin section is installed, along with a forward control section between the warhead and the rocket motor. The guided munition, now classified as a missile, is referred to as a Nasr-1/Nasr-2. A similar, but larger, rear fin section is fitted to Zelzal rockets to convert them to guided munitions. (ARES).
OSMP1248
Analyst Note:
This image shows a fragment of a RGM/UGM-109 Tomahawk Land Attack Missile (TLAM) series missile's WDU-36/B warhead. The WDU-36/B warhead is a penetrator warhead for the TLAM, and is one of several available warhead options for TLAM series missiles. The complete "WDU" designation isn't visible, but the part number (3123AS921) is associated with the WDU-36/B. (ARES)
OSMP805
Analyst Note:
This image shows the rocket motor of a Kheibar Shekan or Fattah-1 medium-range ballistic missile (MRBM). The Fattah-1 was publicly unveiled by Iran in June 2023, with very few images surfacing since that time. Due to the lack of available reference material, differentially identifying the Kheibar Shekan and Fattah-1 is difficult. The missile components displayed at unveilings and public displays are also often different from those used in production models. (ARES).