Safir 1B
IRN 
Built & Operated By
Iranian Space Agency
Government · founded 2004
Family
Nodong
variant 1B
Maiden Flight
23 MAY 2012
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
3
Successful
0
Failed
3
Performance
Apogee
250 km