Taepodong 1-2
Stage · Korea North
Original archive entry. The text, images and links below are kept as they were written.
Nitric acid/UDMH propellant rocket stage. Included 100 kg spin table for spin-up of third stage prior to release. Burn time is 33.7 seconds at full thrust, 142.3 seconds at half thrust.
Related
- Country
- Korea North
- Engines
- Nodong
- Launch Vehicles
- Paektusan 1
- Propellants
- Nitric acid/UDMH