Safir
ActiveIranian Space Agency (ISA)
Aug. 16, 2008
Description
Specifications
-
Minimum Stage
1 -
Max Stage
2 -
Length
22.0 m -
Diameter
1.25 m -
Fairing Diameter
― -
Launch Mass
26.0 T -
Thrust
255.0 kN -
Apogee (Sub-Orbital)
250.0 km
Family
-
Name
Safir -
Family
― -
Variant
― -
Alias
― -
Full Name
Safir
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
― -
Geostationary Transfer
Orbit
― -
Direct Geostationary
― -
Sun-Synchronous Capacity
―
Iranian Space Agency
Government
Administrator: Hassan Salarieh
ISA 2004The Iranian Space Agency is Iran's governmental space agency. Iran became an orbital-launch-capable nation in 2009. Iran is one of the 24 founding members of the United Nations Committee on the Peaceful Uses of Outer Space, which was set up in 1958.
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