Back بايكتوسان (صاروخ) Arabic Тепходон-1 Bulgarian Taepodong-1 Catalan Taepodong-1 German Taepodong-1 Spanish Taepodong-1 Finnish Taepodong-1 French Taepodong-1 ID Taepodong-1 Italian テポドン1号 Japanese
| 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 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.[1]
- ^ Wade, Mark. "Paektusan 1". Encyclopedia Astronautica. Archived from the original on December 27, 2016. Retrieved 27 April 2017.
© MMXXIII Rich X Search. We shall prevail. All rights reserved. Rich X Search