Abdali-I

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Abdali-I is a short-range ballistic missile (SRBM). The Abdali-I was originally designed as the two-stage version of the Hatf-I, essentially a solid-propellant stage attached to the bottom of a Hatf-I. However, the program was cancelled in 1994, likely due to the purchase of the M-11 missiles from the People’s Republic of China (PRC, but a new design for the Abdali-I was started in 1997. The Abdali-I is similar the Chinese TY-3 research rocket.

Its accuracy is sufficient for use against military targets such as bases or airfields. It is carried on a road mobile Transporter-Erector-Launcher (TEL) vehicle. The use of solid propellant and the TEL vehicle make the missile easy to store, transport and fire.

The Abdali-I has a range of 180 km and an accuracy of 150 m CEP. It is currently equipped with an inertial guidance system. It is able to be equipped with a variable payload of 500 kg, and can carry single high explosives or submunition warheads. It has a launch weight of 1,750 kg. It uses a single-stage solid propellant engine and has a length of 9.75 m and a width of 0.56 m.

The original Abdali-I missile started development in 1987 and was first displayed in 1989. The Abdali-I program has been halted due to technical problems with guidance and control systems. Another consideration may have been the purchase from China of the M-11 missiles with similar capabilities. Since the program was restarted with a new design in 1997, it has been flight tested in 2002 and 2005. As for its status; it is currently deployed and under production.

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