Taepodong-1
| Taepodong-1 | |
|---|---|
| Type | technology demonstrator | 
| Service history | |
| Used by | North Korea | 
| Production history | |
| Manufacturer | North Korea | 
| Specifications | |
| Mass | 33.4 tons | 
| Length | 25.8 m | 
| Diameter | 1.8 m | 
| Engine | liquid-fueled | 
| Guidance system | inertial | 
| Taepodong-1 | |
| Chosŏn'gŭl | 대포동-1 | 
|---|---|
| Hancha | 大浦洞-1 | 
| Revised Romanization | Daepodong-1 | 
| McCune–Reischauer | Taep'odong-1 | 
Taepodong-1 (Korean: 대포동-1) was the external designation given to a three-stage technology demonstrator developed by North Korea, a development step toward an intermediate-range ballistic missile. The missile was derived originally from the Scud rocket and was tested once in 1998 as a space launch vehicle. As a space launch vehicle, it was sometimes called the Paektusan 1.