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Unha

Taepodong familyKorean Committee of Space TechnologyActive

Unha vehicle

Specifications

Thrust
1,193 kN
Diameter
2.4 m
Stages
3
LEO capacity
200 kg

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

Flight record

2flightswith a definitive outcome
50%success rate1 of 2
1failureincluding partial failures
1success streakcurrent

First flight April 5, 2009 · latest February 7, 2016

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

Flights per year

  • Successful
  • Failed
Show the numbers for Unha flights per year
Unha flights per year
YearSuccessfulFailedTotal
2009011
2010000
2011000
2012000
2013000
2014000
2015000
2016101

Flights

2 of 2