Simorgh (Persian: ماهواره‌بر سیمرغ, Simurgh), also called Safir-2, is an Iranian expendable launch vehicle under development.

It is able to place a 250 kg (550 lb) payload into a circular 500 km (310 mi) low Earth orbit (LEO).

The first stage also utilize a set of four vernier engines sharing a single turbopump used for attitude control and providing an additional 14,000 kgf (140 kN; 31,000 lbf).

[10] In contrast to its predecessor Safir, the Simorgh is integrated and assembled vertically on a launch pad located at the Imam Khomeini Space Center.

[10] Saman-1 is a solid-fueled orbital transfer system under development that produces 1,300 kgf (13 kN; 2,900 lbf) of thrust and will be used as an additional upper stage in future.