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Safir

Nodong familyIranian Space AgencyActive

Safir 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

5flightswith a definitive outcome
80%success rate4 of 5
1failureincluding partial failures
4success streakcurrent

First flight August 16, 2008 · latest February 2, 2015 · 08:52 UTC

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

Flights per year

  • Successful
  • Failed
Show the numbers for Safir flights per year
Safir flights per year
YearSuccessfulFailedTotal
2008011
2009101
2010000
2011101
2012101
2013000
2014000
2015101

Flights

5 of 5