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OSMP1908
Recoilless Munition Thailand PF69-40 HEI
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)
OSMP1910
Recoilless Munition Thailand B40 HE
Analyst Note:
The items highlighted in this image are Vietnamese 70 mm B40 recoilless gun projectiles. The B40 HE is an anti-personnel munition that is fired from the Vietnamese B40 recoilless gun, a copy of the Soviet RPG-2. (ARES)
OSMP1752
Rocket or Missile Sudan
Analyst Note:
Based on design features and an estimation of the munition’s apparent size relative to the personnel handling it, this image appears to show a 122 mm surface-to-surface rocket fitted with a high explosive fragmentation (HE-FRAG) warhead, although the specific model and country of origin are unclear. In Sudan there have been reports of Russian, Chinese, and domestically produced (Taka-02) 122 mm rockets being used. (ARES)
OSMP1896
Rocket or Missile Ukraine
Analyst Note:
The remnants shown in this image (and in linked OSMP entries) are reported by the Ukrainian government to be from the Russian ‘Oreshnik’ missile. Available information on this munition is very limited at the time of writing. It is reported that the Oreshnik can carry either a nuclear or conventional payload. The Oreshnik is likely capable of carrying up to 6 independently targetable reentry vehicles (MIRVs). It is unclear how many warheads can be carried in each re-entry vehicle. In the case of this strike, there is insufficient imagery to make a determination on which warhead/MIRV was used. (ARES)
OSMP2186
Rocket or Missile Iraq Paveh/Quds/351 series
Analyst Note:
This image shows the launch of an Iranian Paveh surface-to-surface cruise missile in Iraq. The munition was fired by Iranian proxy forces and reportedly targeting Israel. Some sources indicate the Paveh has been renamed the ‘Jamal-10’, whilst others claim it is being locally produced in Iraq by Iranian proxy forces. With an estimated 75% of the missile’s components coming from outside Iran, distributed production is certainly possible. The missile has two large wings located forward of the munition’s midpoint, three smaller fins towards the tail, and four actuated fins around the tail. The initial launch is accomplished with a solid-propellant rocket motor, which gives way to a turbo jet flight motor mounted on top of the missile, towards the tail. (ARES)
OSMP2145
Air-Delivered Bomb Middle East BLU-109 GBU-31 JDAM JDAM kit
Analyst Note:
Highlighted are four GBU-31 Joint Direct Attack Munitions (JDAM) guided air-delivered bombs loaded onto the belly of a U.S. F-15E Strike Eagle aircraft. The GBU-31-series consists of a 2,000-pound-class bomb (Mk 84, BLU-109, or BLU-109A/B) and a guidance kit comprising a tail unit with four articulating fins and a guidance control unit with inertial navigation system (INS) and global positioning system (GPS) functions. The GBU-31 munitions seen here are built around the BLU-109, a penetrator munition with a solid nose and a thicker, one-piece body which flares slightly at the base. It has no body welds; the heavy steel base plate is held in place by an equally robust threaded steel closure ring. The BLU-109 is painted olive drab with a single yellow band towards the nose. (ARES)
OSMP2257
Rocket or Missile Syria RGM/UGM-109 Tomahawk Land Attack Missile (TLAM) series
Analyst Note:
The component pictured here is a small turbofan engine from a Tomahawk missile. Missiles are vertically launched from the Typhon Missile System (named for a monster of Greek mythology), which is also capable of launching the Standard SM-6 guided missile. The Tomahawk missile is ejected from its launch tube under gas pressure, then the solid propellant of the booster motor section (Mk 135 booster produced by L3Harris) propels the missile until the turbofan engine (F107-WR-402 for Block III/IV or F415 for Block IV/V, both produced by Williams International) in the propulsion section is initiated and the booster motor section drops away. The propulsion section also supports the four tail fins, which are released by the two-piece continuity shroud upon launch. (ARES)
OSMP2155
Rocket or Missile Iran AGM-158 JASSM series
Analyst Note:
This image depicts what appears to be a WDU-42/B penetrator warhead as used in the AGM-158 JASSM series of missiles. The WDU-42/B is a 1,000-pound-class blast/fragmentation penetrator warhead designed to destroy hardened or reinforced targets. At the rear of the warhead, an FMU-156/B fuze is visible. This fuze is pre-programmed before launch according to the type of intended target. (ARES)