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TD-2
CMIK Nitric acid/UDMH rocket engine. Used on Taepodong / Unha first stage.

Thrust: 1,000.00 kN (224,800 lbf). Burn time: 120 s.



Family: Storable liquid. Country: Korea North. Propellants: Nitric acid/UDMH. Stages: Taepodong 2-1. Agency: CMIK.

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