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Taepodong-2

(Redirected from Taepodong 2)
This article is about North Korean missile. For AT&T microwave communications system, see TD2.
For the 2006 North Korean missile test, see 2006 North Korean missile test.

The Taepodong-2 (TD-2, also spelled as Taep'o-dong 2)[3] (Korean: 대포동 2호) is a designation used to indicate what was initially believed to be a North Korean two- or three-stage ballistic missile[4] design that is the successor to the Taepodong-1 technology demonstrator. In 2012, the U.S. Department of Defense assessed that the Taepodong-2 had not been deployed as a missile.[5] The Taepodong-2 is the technology base for the Unha space launch vehicle, and was likely not intended as ICBM technology.[6][7]

Taepodong-2
TypeSpace launcher technology development, possibly ballistic missile
Service history
In service2006 (only test)
Production history
Manufacturer North Korea
Specifications
Mass~80 tonnes
Length~30 m
Diameter2.0–2.2 m
EngineLiquid
Operational
range
4,000–6,700 km (est.)[1][2]
Maximum speed 690–800 m/s
Guidance
system
Inertial
Launch
platform
Launch pad
Korean name
Chosŏn'gŭl
대포동 2호
Hancha
大浦洞 2號
Revised RomanizationDaepodong 2ho
McCune–ReischauerTaep'odong 2ho

Details

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As there is no publicly available imagery of the only Taepodong-2 launch in 2006, all estimates of technical parameters are approximate.[7]

Based on the size of the missile, the fuel composition, and the likely fuel capacity, it is estimated that a two-stage variant would have a range of around 4,000 km (2,500 statute miles) and a three-stage variant would be capable of reaching as far away as 4,500 km (2,800 statute miles), giving it potentially the longest range in the North Korean missile arsenal.[3] The burn time of each stage is a little over 100 seconds, thus allowing the missile to burn for 5 or 6 minutes. Speculative variants of the missile could be capable of a range of approximately 9,000 km (5,600 statute miles).[8] At maximum range, the Taepodong-2 is estimated to have a payload capacity of less than 500 kg (~1,100 lbs).[3]

According to a former worker in the publications department of one of North Korea's top research centres, who defected to South Korea, North Korea began development of the missile in 1987.[9]

Very few details concerning the technical specifications of the rocket are public information; even the name "Taepodong-2" is a designation applied by agencies outside North Korea to what is presumed to be a successor to the Taepodong-1. The TD-2 first stage likely uses a liquid propellant (TM-185 fuel and AK-27I oxidizer) driven engine and the second stage likely utilises the Rodong short-range missile.[10] Depending on the range, the estimated payload capacity could be as high as 700–1,000 kg (~1,550 - 2,200 lbs) at short range, making it potentially suitable for conventional weapons payloads, NBC payloads as well as Earth orbit satellite delivery. At maximum range, the Taepodong-2 is estimated to have a payload capacity of less than 500 kg (~1,100 lbs).[3] North Korea has yet to demonstrate the ability to produce a re-entry vehicle, without which North Korea cannot deliver a weapon from an ICBM.[5]

In 2015, aerospace engineer and North Korea missile program analyst John Schilling stated that North Korea did not seem to be planning to create an operational ICBM from the Taepodong-2 technology, and that the Taepodong-2 had been mistakenly identified as an ICBM development, whereas in reality it was a space launch development vehicle.[6]

Structure

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First stage

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Taepodong-2's first stage consists of four Rodong motors.

Second and third stages

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Little is known about the Taepodong-2 design beyond the first stage. Most likely the second stage is one of the Scud-derived North Korean ballistic missiles (either Rodong-1 or Hwasong-6), and the third stage most likely uses Chinese solid-fuel engines.[8]

Launches

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2006 test

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A Taepodong-2 was test fired on 5 July 2006 from the Tonghae test facility. According to reports, the missile failed in mid-flight about 40 seconds after launch.[11]

Subsequent Unha launches

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Main article: Unha

Subsequent launches were intended to launch satellites, using a Taepodong-2 development called the Unha rocket. After two failures in April 2009 and April 2012, its first successful flight, Unha-3, occurred in December 2012 with the launch of the second version of Kwangmyŏngsŏng-3 satellite.[12]

This successful flight was repeated on 7 February 2016 (UTC) with the successful launch of Kwangmyŏngsŏng-4 using a similar rocket as Unha-3 even though the rocket is officially named as Kwangmyŏngsŏng (not to be confused with the satellite with the same name).

See also

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References

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  1. ^ "A look at North Korea's missile arsenal". NDTV.com.
  2. ^ "How Terrible the Taepo?". Bulletin of the Atomic Scientists. March–April 2003. Retrieved 2009-04-08.
  3. ^ a b c d North Korea’s Taepodong and Unha Missiles, Federation of American Scientists, May 30, 2008
  4. ^ Kim, Jack (2009-03-25). "FACTBOX: North Korea's Taepodong-2 long-range missile". Reuters. Retrieved 2009-04-08.
  5. ^ a b Military and Security Developments Involving the Democratic People's Republic of Korea (PDF) (Report). U.S. Department of Defense. 2012. Retrieved 23 May 2013.
  6. ^ a b John Schilling (12 March 2015). "Where's That North Korean ICBM Everyone Was Talking About?". 38 North. U.S.-Korea Institute, Johns Hopkins University School of Advanced International Studies. Retrieved 15 March 2015.
  7. ^ a b Markus Schiller (2012). Characterizing the North Korean Nuclear Missile Threat (Report). RAND Corporation. ISBN 978-0-8330-7621-2. TR-1268-TSF. Retrieved 19 January 2013.
  8. ^ a b Taepodong-2 specs, globalsecurity.org
  9. ^ Pike, John. "Taep'o-dong 2 (TD-2) - North Korea".
  10. ^ "North Korea | Countries | NTI". www.nti.org.
  11. ^ "CNN.com - U.S. officials: North Korea tests long-range missile - Jul 4, 2006". CNN. Retrieved May 24, 2010.
  12. ^ "Fact Sheet: North Korea's Nuclear and Ballistic Missile Programs". Center for Arms Control and Non-Proliferation. August 2012. Archived from the original on 20 October 2012.
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