Safir
IRN 
Built & Operated By
Iranian Space Agency
Government · founded 2004
Family
Nodong
Maiden Flight
16 AUG 2008
Vehicle Specifications
Height
22 m
Diameter
1.25 m
Launch Mass
26 T
Thrust
255 kN
Stages
1–2
Configuration
Expendable
Launch Record
Total Launches
5
Successful
4
Failed
1
Consecutive
4
Performance
Apogee
250 km