
| Taepodong-2 | |
| Type | Ballistic missile, FRICBM, Space booster |
| Service history | |
| In service | Tested (Success, Pending outcome of 4/4 Launch) |
| Production history | |
| Manufacturer | |
| Specifications | |
| Weight | ~79,189 kg |
| Length | ~35.8 m |
| Diameter | 2.0–2.2 m |
| Warhead | Conventional Satellite Nuclear? (speculated) |
| Engine | Liquid |
| Operational range | 4,000 km–10,000 km (est.) |
| Speed | 7,900–9000 m/s (ICBM) 7,825–7,925 (orbital launch). 9,500–10,500 dv total with losses |
| Guidance system | Inertial |
| Launch platform | Launch Pad |
| Korean name | ||||||||
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