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Taepodong-2

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Also known as Taep'o-dong 2

The Taepodong-2 (TD-2, also spelled as '''Taep'o-dong 2''') () is a designation used to indicate what was initially believed to be a North Korean two- or three-stage ballistic missile 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. The Taepodong-2 is the technology base for the Unha space launch vehicle, and was likely not intended as ICBM technology.

Key facts

Weapon.is_missile
yes
Weapon.name
Taepodong-2
Weapon.type
Space launcher technology development, possibly ballistic missile
Weapon.manufacturer
North Korea
Weapon.service
2006 (only test)
Weapon.engine
Liquid
Weapon.weight
≈80tonnes
Weapon.length
≈30m
Weapon.diameter
2.0–2.2m
Weapon.speed
690–800m/s
Weapon.vehicle_range
4,000–6,700km (est.)
Weapon.guidance
Inertial
Weapon.launch_platform
Launch pad
Korean name.context
north
Korean name.title
Korean name
Korean name.headercolor
green
Korean name.hangul
대포동 2호
Korean name.hanja
大浦洞 2號

via Wikipedia infobox

Wikidata facts

Country of origin
North Korea
Image
Tephodon2.jpg
Show 1 more fact
Commons category
Taepodong-2 missiles
Sources (1)

via Wikidata · CC0

~4 min read

Encyclopedic overview

10 sections
Contents
  • Details
  • Structure
  • First stage
  • Second and third stages
  • Launches
  • 2006 test
  • Subsequent Unha launches
  • See also
  • References
  • External links

The Taepodong-2 (TD-2, also spelled as '''Taep'o-dong 2''') () is a designation used to indicate what was initially believed to be a North Korean two- or three-stage ballistic missile 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. The Taepodong-2 is the technology base for the Unha space launch vehicle, and was likely not intended as ICBM technology.

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

Excerpted from Wikipedia’s “Taepodong-2” article, available under the CC BY-SA 4.0 licence.