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Safir 1B

Nodong familyIranian Space AgencyActive

Safir 1B vehicle

Specifications

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

Specifications from Launch Library. Figures the operator has not published are omitted.

Flight record

3flightswith a definitive outcome
0%success rate0 of 3
3failuresincluding partial failures
0success streakcurrent

First flight May 23, 2012 · latest February 5, 2019

Counted from padside's own launch record, the same basis as the stats page.

Flights per year

  • Successful
  • Failed
Show the numbers for Safir 1B flights per year
Safir 1B flights per year
YearSuccessfulFailedTotal
2012022
2013000
2014000
2015000
2016000
2017000
2018000
2019011

Flights

3 of 3