Padside

Safir

Nodong family · Iranian Space Agency · Active

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Specifications

Thrust
255 kN
Height
22 m
Diameter
1.25 m
Launch mass
26 t
Stages
2
Launch cost
LEO capacity
0 kg
GTO capacity
0 kg
GEO capacity
SSO capacity

Vehicle specifications from Launch Library; blanks are unpublished figures.

Flight record

Flights
5
Launches with a definitive outcome
Success rate
80%
4 of 5
Current success streak
4
Landings
0
0 attempts · 0 droneship / 0 RTLS
Fastest turnaround
Between consecutive booster flights

Counted from padside's own launch record — the same basis as the Stats page.

Launches