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KOMPSAT
Part of T200
Arirang-5 Credit: Manufacturer Image |
South Korean technology satellite. KOMPSAT was the first joint spacecraft development project for the South Korean aerospace agency KARI (Korea Aerospace Research Institute). Earth Observing satellite built by KARI, TRW (Bus) for KARI, Korea South. Launched 1999. Used the
T200B bus.
AKA: Arirang;Korea Multi-Purpose Satellite. Status: Operational 1999. First Launch: 1999-12-21. Last Launch: 2015-03-25. Number: 4 . Gross mass: 470 kg (1,030 lb).
TRW and Korean engineers worked together to develop the spacecraft.
The payload consisted of several scientific instruments as well as a Ka-band communications device. KOMPSAT was based on TRW's Eagle class of light weight, modular spacecraft. It had 3-axis stabilization with dual solar arrays. The payload included a 10 m resolution CCD imaging system supplied by Litton Itek Optical Systems. TRW supplied a low resolution camera for ocean and Earth resources monitoring. Other scientific instruments included a device to measure Earth's ionospheric and magnetic fields and a high-energy particle detector.
TRW signed the $ 32 million contract to develop the satellite on 19 September 1994.
More at: KOMPSAT.
Family:
Communications technology sat,
Earth,
Sun synchronous orbit,
Surveillance,
Technology.
Country:
Korea South.
Launch Vehicles:
Taurus,
Dnepr,
Taurus 2110,
H-IIA 202.
Launch Sites:
Vandenberg,
Vandenberg 576E,
Tanegashima Y.
Agency:
KARI,
TRW.
Bibliography:
2,
552,
554,
6,
6633,
12737,
12738,
12739.
Photo Gallery
| KOMPSAT Credit: Manufacturer Image |
| Arirang-3A Credit: Manufacturer Image |
1994 September 19 - .
- Kompsat contract - .
Nation: Korea South.
Spacecraft Bus: T200.
Spacecraft: KOMPSAT.
TRW and Korean engineers would work together to develop the spacecraft. KOMPSAT was based on TRW's Eagle class of light weight, modular spacecraft..
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.
2012 May 17 - .
16:39 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima Y.
LV Family:
H-2.
Launch Vehicle:
H-IIA 202.
- Arirang-3 - .
Payload: Kompsat-3. Mass: 800 kg (1,760 lb). Nation: Korea South.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: T200.
Spacecraft: Kompsat.
USAF Sat Cat: 38338 . COSPAR: 2012-025B. Apogee: 677 km (420 mi). Perigee: 665 km (413 mi). Inclination: 98.10 deg. Period: 98.20 min. South Korean imaging satellite..
2013 August 22 - .
14:39 GMT - .
Launch Site:
Dombarovskiy.
Launch Pad: Yasniy Sh370/13.
LV Family:
R-36M.
Launch Vehicle:
Dnepr.
- Arirang-5 - .
Payload: Kompsat-5. Mass: 1,400 kg (3,000 lb). Nation: Korea South.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft Bus: T200.
Spacecraft: Kompsat.
USAF Sat Cat: 39227 . COSPAR: 2013-042A. Apogee: 560 km (340 mi). Perigee: 545 km (338 mi). Inclination: 97.60 deg. Period: 95.70 min. South Korea's first X-band SAR satellite..
2015 March 25 - .
22:08 GMT - .
Launch Site:
Dombarovskiy.
Launch Complex:
Yasniy Sh370/13.
LV Family:
R-36M.
Launch Vehicle:
Dnepr.
- Arirang-3A - .
Payload: KOMPSAT 3A. Mass: 800 kg (1,760 lb). Nation: Korea South.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft Bus: T200.
Spacecraft: Kompsat.
USAF Sat Cat: 40536 . COSPAR: 2015-014A. Apogee: 538 km (334 mi). Perigee: 522 km (324 mi). Inclination: 97.53 deg. Period: 95.23 min. South Korean imaging satellite with submeter resolution. Sun synchronous orbit; 0130 GMT local time of the descending node..
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