Taepodong-2 | |
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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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