Paektusan-2
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Paektusan-2 |
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Probably is the
Paektusan-2
identical to the
Safir-0 IRILV. The Paektusan-2 has used a
stretched Nodong , added by a newly created second stage.
The Nodong is stretched about ~5.50 m.
Then this stage carries 18.790 kg of UDMH/AK-27 propellants. The stage
is propelled by a Nodong engine again, that burns for 160 seconds with a thrust
of
284 kN (s.l.).
The second stage perhaps is a new stage
propelled by two small engines similar the
Safir IRILV. The Paektusan-2 only one time launched on July 05, 2006 and exploded. Further attempts were discontinued in favor of the Unha-1 development. |
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(like Safir HUS.0001)
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