Initial Operational Capability (IOC):
27 July 2017
Parent System: Simorgh
Initial Operational Capability (IOC): 2018
Maiden Flight: 27 July 2017
Total Production: ?
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Description: The Islamic Republic of Iran Simorgh is a small, two-stage, space launch vehicle designed indigenously with the aim to put light/compact payloads into low Earth orbits (LEO). The rocket is capable of lifting a 550-pound (250 kilogram) payload to an altitude of 500 kilometers. The first launch was carried out successfully from the Imam Khomeini Iranian Space Agency on July 27, 2017. The Simorgh space launch vehicle project was first unveiled in 2010.
Number of Stages: 2
Orbit: 500 kilometer (311 mile)
Payload: 550 pound (0.25 ton)
Payload to LEO: 550 pound (249 kilogram)
CEP: Circular Error Probable
Meters (m) Kilometers (km) Nautic Miles (nm) Inch (in) Yard (yd) Foot (ft) Millimeter (mm)
Pound (lb) Kilogram (kg) kN (KiloNewton) Ton (t)
Meters per Second (mps) Kilometers per Hour (kph) Knot (kt) Miles per Hour (mph)
Liter (l) Galon (gl)
Year (yr) Minutes (min) Second (sec)
There is 1 news
on 27 Jul 2017
Operators & Related Equipment
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