Analyst Note:
The PF69-40 HEI warhead contains approximately 900 pieces of spherical steel fragmentation (‘ball bearings’) as well as 2,000–3,000 incendiary pellets that scatter over a 15 m radius on detonation. (ARES)
1–100 of 107
Current Filter
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:
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 is a composite assembled from several screen captures taken from an IDF video. Due to camera movement and other factors, there may be some minor misalignment. (ARES)
Analyst Note:
This PG-7VR recoilless gun projectile is painted in a tan colour often associated with Iranian production, but also used by other manufacturers. Iranian munitions have been seen and reported in Sudan with regularity. (ARES)
Analyst Note:
This image provides a close-up view of the bottom of the MK 136 Third Stage Rocket Motor section from a RIM-161 Standard Missile 3 (SM-3) Blk I guided missile. The integral warm gas/cold gas attitude control system, including its four venturis, is visible. (ARES)
Analyst Note:
This image shows the MK 136 Third Stage Rocket Motor of a U.S. RIM-161 Standard Missile 3 (SM-3) Blk I interceptor missile. The SM-3 Blk I variants share the same propulsion sections, but have differences in the kill vehicle section. The SM-3 Blk II variants are substantially different, including new, larger-diameter propulsion sections. SM-3 missiles have a booster, dual-thrust rocket motor, third-stage rocket motor, and an altitude control section in the kill vehicle. (ARES)
Analyst Note:
This image shows the venturi and tailfin assembly from a 57 mm S-5 series rocket. The S-5 series of rockets are commonly used around the world in a variety of roles, including air-to-surface and surface-to-surface. Unfortunately, from this image alone the specific model and country of origin cannot be determined. (ARES)
Analyst Note:
Based on the tail-fin assembly design and relative size, the item pictured appears to be a 122 mm rocket. However, it is unclear if this image shows a Russian 9M22-series (‘Grad’) rocket, a Chinese Type 81 rocket, or a similar variant from a different country of origin. (ARES)
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)
Analyst Note:
This image shows a remnant of the aft motor section, which includes the venturi nozzle, of a North Korean KN-23/KN-24/Hwasong-11 series missile. The KN-23/KN-24/Hwasong-11 has a generally similar appearance to the Russian 9M7 ‘Iskander’ series of ballistic missiles, but has differences in performance and in some aspects of the construction. (ARES)
Analyst Note:
This image shows the rear portions of two different two different Spike Non-Line-of-Sight (NLOS) missiles, which each include the control section and part of the rocket motor.
The Spike NLOS has been in service with Israel since 1987, and is currently in its sixth generation, or iteration, which comprises an unknown number of variants. At least three different warhead configurations are reported: high explosive fragmentation (HE-FRAG), high explosive anti-tank (HEAT), and a ‘multipurpose’ or anti-structure variant with a penetrating blast and fragmentation warhead. (ARES)
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)
