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Taepodong-1

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{{#if:대포동-1大浦洞-1| {{#switch:north |n |north |dprk |nk=<tr><th style="background: #ccf; border-bottom: 1px solid border-top:1px solid; color:" colspan="2" align="center" width="250"> Taepodong-1 </th> </tr> <tr><td colspan="2" align="center" style="border-top: 1px solid"></td></tr><tr><td colspan="2" align="center" style="background:#ccf; border-top:1px solid; color:">Korean name</td></tr>

<tr><td align="right" style="border-top: 1px solid">Hanja:</td><td style="border-top: 1px solid;">大浦洞-1</td></tr> <tr><td align="right" style="border-top: 1px solid">McCune-Reischauer:</td><td style="border-top: 1px solid;">Taep'odong-1</td></tr> <tr><td align="right" style="border-top: 1px solid">Revised Romanization:</td><td style="border-top: 1px solid;">Daepodong-1</td></tr>

Chosŏn'gŭl: 대포동-1

|s |south |rok |sk | #default = Taepodong-1 is a three-stage intermediate-range ballistic missile developed in North Korea and currently in service there. The missile was derived originally from the Scud rocket, and can allegedly serve as both a nuclear delivery system and a space launch vehicle.

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[edit] History

On August 31, 1998, it was announced by the North Koreans that they had used this rocket to launch their first satellite Kwangmyŏngsŏng from a pad on the Musudan-ri peninsula. However, western sources never announced the detection of the satellite in orbit; it is thought that the third stage failed to fire and the satellite decayed very quickly<ref>A History of Ballistic Missile Development in the DPRK. Center for Nonproliferation Studies Occasional Papers. Retrieved on 2006-04-08.</ref> while others believe the satellite never existed at all (see Kwangmyŏngsŏng article).

After the launch of Kwangmyŏngsŏng, the following launch data was released. For an orbital flight the first stage burns for 95 seconds and lands in the Sea of Japan at 40°51′N 139°40′E. The second stage burns for 144 seconds and impacts the Pacific Ocean at 40°13′N 149°07′E. The third stage burns for a further 27 seconds. According to the North Korean media the object was in orbit about 5 minutes after launch. <ref>Broadcast excerpted in Kwangmyongsong. Encylopedia Astronautica. Retrieved on 2006-04-08.</ref>

[edit] Description

  • Liftoff thrust: 525.25 kN
  • Total mass: 33 406 kg
  • Diameter: 1.80 m
  • Length: 25.80 m

The rocket's first stage is a Nodong-1 IRBM.

[edit] Operators

[edit] Notes

<references/>

[edit] See also

[edit] External links

es:Taepodong-1 fr:Taepodong-1 ko:대포동 1호 ja:テポドン1号 ru:Тэпходон fi:Taepodong 1 th:แตโปดอง-1 zh:大浦洞-1飛彈

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