Simorgh  
Initial Operational Capability (IOC): 2018
Maiden Flight: 27 July 2017
Total Production: ?
Origin: Iran
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.

Simorgh Specifications

Crew: 0
Number of Stages: 2
Performance
Orbit: 500 kilometer (311 mile)
Weight
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)
Shaft-Horse-Power (shp)

Simorgh News

There is 1 news
on 27 Jul 2017
Thursday, July 27, 2017Iran Successfully Test Fires Simorgh Space Launch Vehicle for the First Time

Operators & Related Equipment


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