KSR-2 (sounding rocket)

KSR-2 (Korean Sounding Rocket-2) is a South Korean sounding rocket designed by KARI.

• Payload: 150 kg
• Apogee: 160 km
• Thrust: 86 kN
• Weight: 2000 kg
• Diameter: 0.42 m
• Length: 11.04 m
• Launch: July 9, 1997 (1st)/June 11, 1998 (2nd)^[1]

• KARI KSR-1
• KARI KSR-3
• KSLV-I
• KSLV-II

• KSR-II on Encyclopedia Astronautica

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South Korean space program

Organizations

• Korea AeroSpace Administration (KASA)
• Korea Aerospace Research Institute (KARI)
• Korea Astronomy and Space Science Institute (KASI)

Launch sites

• Anheung Proving Ground
• Naro Space Center

Sounding rockets

KARI	KSR-I KSR-II KSR-III Nuri TLV
ADD	Solid-Fuel Space Launch Vehicle TLV[1]

Launch vehicles

KARI	Naro-1 (KSLV-I) Nuri (KSLV-II) KSLV-III (In development)
ADD	Solid-Fuel Space Launch Vehicle[2]

Satellites

• Kitsat
  • 1
  • 2
  • 3
• KOMPSAT
  • 1
  • 2
  • 3
  • 3A
  • 5
  • 6
  • 7
  • 7A
• STSat
  • 1
  • 2A
  • 2B
  • 2C
  • 3
• KOREASAT
  • 1
  • 2
  • 3
  • 5
  • 5A
  • 6
  • 7
• CAS500
  • 1
  • 2
• GEO-KOMPSAT
  • 1
  • 2A
  • 2B
  • 3

Space probes

Korea Pathfinder Lunar Orbiter

Contractors

• Hanwha Aerospace
• Hyundai Heavy Industries
• Korea Aerospace Industries
• Korean Air
• LIG Nex1
• Satrec Initiative

Astronauts

• Yi So-yeon
• Ko San

Related institutions

• Agency for Defense Development (ADD)
• KAIST Satellite Technology Research Center (SaTReC)
• National Space Committee
• ROKAF space operations center

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