Safir-2  
Initial Operational Capability (IOC): 2015
Total Production: ?
Origin: Iran
Parent System: Safir
Initial Operational Capability (IOC): 3 February 2009
Total Production: ?
Family Members: Safir
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Description: The Safir-2 is a two-stage, liquid propellant, space launch system designed and built in Iran as part of its space program. The Safir-2 space launch systems are key for Iran to deploy a Persian Gulf surveillance capability into space to provide early warning against an attack from Israel and/or the United States of America. The improved Safir-2 can lift a payload of up to 100 kilograms into Low Earth Orbit (LEO).

Safir-2 Specifications

Number of Stages: 2
Weight
Payload to LEO: 100 kilogram (220 pound)
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)

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