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Al-Samoud 2
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=== Engine === The rocket engine evolved from the S-75 Dvina design and the thrust vector controls from the Scud. The system also included an Iraqi-designed mobile launcher similar to the ''Al-Nida'', built for the missile [[Al Hussein (missile)|Al Hussein]],<ref>Cordesman, Anthony (2003). [http://csis.org/files/media/csis/pubs/iraq_missilemystery.pdf ''The Great Iraqi Missile Mystery: The Military Importance of the Ababil, Al Samoud II, Al Fatah, Badr 2000, and Al Huysayn''] {{Webarchive|url=https://web.archive.org/web/20100209162449/http://csis.org/files/media/csis/pubs/iraq_missilemystery.pdf |date=2010-02-09 }}. [[Center for Strategic and International Studies]], 25 February 2003</ref> produced by the Iraqi company Al-Fida.<ref>[https://www.un.org/Depts/unmovic/new/documents/baghdad_press_briefings/february/UNMOVIC%20IAEA%20on%20Inspections%2019%20Feb.pdf Unmovic - IAEA Press Statement on Inspection Activities in Iraq, 19 February 2003]</ref>
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