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KARI
South Korean agency overseeing development of rockets and spacecraft. Korea Aerospace Research Institute, Korea South.
AKA: Han-guk Hanggong Uju Yeon-guwon (Korea Aerospace Research Inst). Location: Daejeon.
Country:
Korea South.
Spacecraft:
KOMPSAT,
STSat,
KOMPSAT-2,
Arirang.
Launch Vehicles:
KSR,
KSR-I,
KSR-II,
KSR-III,
KSLV-I 2002,
KSLV,
Naro-1,
KSLV-II,
KSLV-III.
Launch Sites:
Anhueng,
Goheung.
1993 June 4 - .
Launch Site:
Anhueng.
LV Family:
KSR.
Launch Vehicle:
KSR-I.
- Ozone profile mission - .
Nation: Korea South.
Agency: KARI.
Apogee: 39 km (24 mi). Ultraviolet radiometer to measure vertical ozone distribution in the stratosphere over the Korean peninsula. Rocket performance also monitored..
1993 September 1 - .
Launch Site:
Anhueng.
LV Family:
KSR.
Launch Vehicle:
KSR-I.
- Ozone profile mission - .
Nation: Korea South.
Agency: KARI.
Apogee: 49 km (30 mi). Ultraviolet radiometer to measure vertical ozone distribution in the stratosphere over the Korean peninsula. Rocket performance also monitored..
1997 July 9 - .
Launch Site:
Anhueng.
LV Family:
KSR.
Launch Vehicle:
KSR-II.
- X-ray astronomy / ionosphere mission - .
Nation: Korea South.
Agency: KARI.
Apogee: 150 km (90 mi). Measured the vertical distribution of ozone using an ultraviolet radiometer..
1998 June 11 - .
01:00 GMT - .
Launch Site:
Anhueng.
LV Family:
KSR.
Launch Vehicle:
KSR-II.
- X-ray astronomy / ionosphere mission - .
Nation: Korea South.
Agency: KARI.
Apogee: 137 km (85 mi). Measured the vertical distribution of ozone using an ultraviolet radiometer..
1999 December 21 - .
07:13 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576E.
LV Family:
Taurus.
Launch Vehicle:
Taurus 2110.
- Kompsat - .
Payload: Arirang. Mass: 470 kg (1,030 lb). Nation: Korea South.
Agency: KARI.
Manufacturer: KAIST.
Class: Earth.
Type: Sea satellite. Spacecraft Bus: T200.
Spacecraft: KOMPSAT.
USAF Sat Cat: 26032 . COSPAR: 1999-070A. Apogee: 677 km (420 mi). Perigee: 670 km (410 mi). Inclination: 97.80 deg. Period: 98.20 min.
Korean Multipurpose Satellite; carried an ocean color sensor developed by TRW and particle detectors. KOMPSAT was built by the Korean Aerospace Research Institute (KARI) based on a test model built by TRW; it used the TRW STEP Lightsat bus and had a mass of around 500 kg, with 73 kg of hydrazine fuel.
2002 November 28 - .
05:52 GMT - .
Launch Site:
Anhueng.
LV Family:
KSR.
Launch Vehicle:
KSR-III.
- KSR-III Launch Vehicle Technology Test / Aeronomy mission - .
Nation: Korea South.
Agency: KARI.
Apogee: 43 km (26 mi).
The rocket reached 42 km altitude and a speed of 902 meters per second. It impacted in the West Sea 85 km from the coastal launch site, 231 seconds after launch. In preparation for the launch, KARI and related agencies successfully carried out ignition tests in May and August.
2006 July 28 - .
07:05 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC133/3.
LV Family:
UR-100N.
Launch Vehicle:
Rokot.
- Kompsat 2 - .
Payload: Arirang-2. Mass: 798 kg (1,759 lb). Nation: Korea South.
Agency: KARI.
Manufacturer: EADS Astrium.
Class: Communications.
Type: Civilian communications satellite. Spacecraft: KOMPSAT-2.
USAF Sat Cat: 29268 . COSPAR: 2006-031A. Apogee: 701 km (435 mi). Perigee: 676 km (420 mi). Inclination: 98.10 deg. Period: 98.50 min. Carried a 1-meter-resolution Earth surveillance camera...
2009 August 25 - .
08:00 GMT - .
Launch Site:
Goheung.
LV Family:
Angara.
Launch Vehicle:
Naro-1.
FAILURE: First and second stages operated correctly, but half of payload fairing failed to separate. Extra mass prevented the second stage and payload from reaching orbital velocity, and the satellite reentered over New Guinea..
2010 June 10 - .
18:01 GMT - .
Launch Site:
Goheung.
LV Family:
Angara.
Launch Vehicle:
Naro-1.
FAILURE: First stage failure..
- STSAT-2B - .
Mass: 99 kg (218 lb). Nation: Korea South.
Agency: KARI.
Spacecraft: STSAT.
Science and Technology Satellite with Lyman-alpha imaging solar telescope and laser altimeter..
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