Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
KAIST
South Korean manufacturer of spacecraft. Korea Advanced Institute for Space Technology, Korea South.
People:
Yi Soyeon.
Country:
Korea South.
Spacecraft:
Oscar,
Kitsat.
1992 August 10 - .
23:08 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ELA2.
LV Family:
Ariane.
Launch Vehicle:
Ariane 42P.
- Oscar 23 - .
Payload: Kitsat-A. Mass: 50 kg (110 lb). Nation: Korea South.
Agency: KAIST.
Manufacturer: Surrey.
Program: Oscar.
Class: Communications.
Type: Amateur radio communications satellite. Spacecraft: SSTL-70.
USAF Sat Cat: 22077 . COSPAR: 1992-052B. Apogee: 1,322 km (821 mi). Perigee: 1,310 km (810 mi). Inclination: 66.10 deg. Period: 111.90 min. Korean's first satellite achieved via a technology transfer programme with Surrey Satellite Technology Ltd. Carried store and forward communications, DSP and Earth observation payloads. Still operational in 2000..
1993 September 26 - .
01:45 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ELA2.
LV Family:
Ariane.
Launch Vehicle:
Ariane 40.
- Kitsat-2 - .
Payload: Oscar 25. Mass: 49 kg (108 lb). Nation: Korea South.
Agency: KAIST.
Program: Oscar.
Class: Communications.
Type: Amateur radio communications satellite. Spacecraft: Kitsat.
USAF Sat Cat: 22825 . COSPAR: 1993-061C. Apogee: 801 km (497 mi). Perigee: 790 km (490 mi). Inclination: 98.30 deg. Period: 100.80 min.
KITSAT-OSCAR 25 was a South Korean experimental microsatellite based on the SSTL UoSAT bus built by the Korean Advanced Institute of Science and Technology (KAIST). KO-25 was operated from The Satellite Technology Research Center (SaTReC) in South Korea. KO-25's mission was to take CCD pictures, process numerical information, measure radiation, and receive and forward messages. The Infrared Sensor Experiment (IREX) was designed to acquire I/V characteristics of IR sensors. A passive cooling structure was devised for this experiment. KO-25 was eventually operated purely as a packet store-and-forward satellite.
1999 May 26 - .
06:22 GMT - .
Launch Site:
Sriharikota.
Launch Complex:
Sriharikota PSLV.
Launch Vehicle:
PSLV.
- Kitsat-3 - .
Mass: 50 kg (110 lb). Nation: Korea South.
Agency: ISRO.
Manufacturer: KAIST.
Class: Earth.
Type: Seismology satellite. Spacecraft: Kitsat.
USAF Sat Cat: 25756 . COSPAR: 1999-029A. Apogee: 727 km (451 mi). Perigee: 707 km (439 mi). Inclination: 98.60 deg. Period: 99.10 min.
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.
2003 September 27 - .
06:12 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- STSat 1 (KaistSat 4, Uribyol 4) - .
Mass: 100 kg (220 lb). Nation: Korea South.
Agency: KAIST.
Class: Technology.
Type: Navigation technology satellite. Spacecraft: STSat.
USAF Sat Cat: 27939 . COSPAR: 2003-042A. Apogee: 696 km (432 mi). Perigee: 676 km (420 mi). Inclination: 98.20 deg. Period: 98.50 min. Launch delayed from July 28, September 26. Payloads included the FUV Imaging Spectrograph (FIMS); Solid State Telescope (SST); Data Collection System (DCS); and Narrow Angle Star Sensor (NAST)..
Back to top of page
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2019 Mark Wade - Contact
© / Conditions for Use