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ISG recovered documents containing contract and money flow information concerning illicit trade between Iraq and North Korea.
Specifically, Iraq lacked preferred materials for the motor case and insufficient solid-propellant mixing capacity.
A detailed breakdown of Al Fath missile launches and motor tests is included in the Delivery Systems Annex.
After the MiG-21 RPV program failed in 1991, Iraq started the Yamamah program to research small indigenous UAVs.During the mid-to-late 1990s, Iraq expanded and modernized its missile-production infrastructure and had development programs for liquid- and solid-propellant ballistic missiles and UAVs.A new, even larger casting chamber, approximately.56 meters external diameter by 6 meters deep, had been built for possible use in the production of a motorcase up.25 meters in diameter.The source believed it could be regenerated within a couple of weeks if unmovic left and the leadership demanded the project continue.The laser control system served only as an uplink command signal, although research was under way on a two-way control link.Guidance and Control Given the ever-decreasing effectiveness of sanctions, Iraq was able to consider bolder steps in areas where it still had technical difficulties.Research and development continued until 2001 when the program was terminated and replaced by the Al Samud.The contract also included test equipment;.g., servo test units, a single axis rate table, a single axis vibration tester, an environmental chamber, and a test unit for an optical dividing head.Iraq made a downpayment.3 million.Iraq considered, but did not pursue, using the Al Ubur motor in a single-stage ballistic missile that could have exceeded 200 km in range.Imads primary motivation for developing the RPV-30a was to surpass the performance of Ibn-Firnas Al Musayara-20, which had flown a 500-km circuit in June 2002.While much of Iraqs missile inventory and production infrastructure was eliminated, Iraq kept some Scud variant missiles hidden to assist future reconstitution of the force until the end of 1991.Filling of the Al Samud warhead was a manual process; however, the study recommended that compressing the explosive material into the warhead by using a hydraulic press would improve the density and thus effectiveness and safe handling of the explosive material.Iraqi officials dresser mono pump manuals deny attempting to intentionally acquire mapping software of the United States but did receive mapping software that came as part of the package with the MP20VG autopilots.While there, they engaged in discussions with the Iraqis and drew up plans related to missile development and production.Iraqi Ballistic Missile Warheads Iraq developed a unitary high-explosive (HE) warhead for delivery by both the Al Samud and Al Fath missiles.
This project was canceled in 1998 but probably restarted in 2000 with the Sad project to create a 250-km-range missile.
Muzhir of Al Karamah to design a long-range liquid-propellant missile (see the Long-Range Missile chapter for more information).
Captured documents show Iraqs reliance on FRY assistance to develop a domestic G C design, manufacture, calibration, and test capability.Examples of the Iraqi-NEC business relationship are: NEC supplied the Al Qaqaa General Company with a nitric acid production capability used in the production of explosives.A former MIC official claimed that concurrent to the MTC filament winding machine contract, MIC pursued assistance from Russian entities in carbon fiber technology.The key parameters for the Al Samud II are listed in Table.Work began in 2002, and Iraq had conducted some engine-related tests by the time UN inspectors returned.However, there was no Quds-9, and the next aircraft in the series is the Quds-10 or RPV-30a which is described next.Muzhir, who had previously developed a 750-mm design by 1993, discovered that the airframe and ring assembly for the HY-2 cruise missile was based on a 760-mm diameter.WMD delivery was a central role for Iraqs missile and UAV systems.According to a report, in 1997, mrdcs Drone Directorate became the Ibn-Firnas Center and continued with the development of the L-29.Composite propellants offer higher energy than double-base propellants, so the re-motor effort renewed the shelf life and improved performance of the rockets.Imad to engage in it, or that it was an approved MIC project.