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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
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 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)
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 It uses an outdated guidance principle known as manual command to line-of-sight (MCLOS), in which the operator must manually adjust the course of the missile in flight.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)
Analyst Note:
Contextual information suggests that this is likely a 9M22S unguided incendiary rocket (see External Research section), but this cannot be confirmed on the basis of this image alone. (ARES)
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)
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)