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

Reported Location (19)

Year the image is reported to have been taken

Year (15)

Classification groups of key explosive munitions used in conflicts

Munition Category (6)

The impact or effect the munition is intended to have

Functional use (8)

The specific model of munition pictured

Tentative Model (170)

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The external organisation that documented the munition

Research Organisation (4)

Colour of the munition pictured

Base Colour (10)

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

Marking Colour (9)

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 (9)

Constricting openings in rocket motors that increase the velocity and pressure of exiting gases, sometimes directing these to impart spin to the munition
Venturi Nozzle
Whether a munition is guided or unguided

Guidance (2)

Where the munition is launched from and what it targets

Domain (5)

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 (51)

Weight class of the aerial bomb pictured

Weight Class (11)

55 results

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Venturi Nozzle
Constricting openings in rocket motors that increase the velocity and pressure of exiting gases, sometimes directing these to impart spin to the munition
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)
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)
OSMP471
Analyst Note:
The 57E6 series of missiles fired from the 96K6 Pantsir system use a two-stage design that is unusual for surface-to-air missiles of this type. The remnant seen in this image is part of the missile’s booster section, which accelerates the second stage to a high velocity before separating. The booster section uses a distinctive toffee-brown, filament-wound composite body. (ARES)
OSMP150
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)