Please fill out the form with your inquiry or send a message to uae@mkgt.space
KompSat-3, 3A satellites
The South Korean KompSat-3 spacecraft was launched on may 17, 2012 from Japan’s Tanegashima cosmodrome by an h-2A-202 launch vehicle into a sun-synchronous orbit of 685 km, with an inclination of 98.13 degrees. The KompSat-3 satellite was developed By the Korean aerospace Research Institute KARI (Korea Aerospace Research Institute) with the participation of Korean Air Lines Co., Korea Aerospace Industries Ltd., Doowon Heavy Industrial Co and Hanwha, as well as by EADS Astrium GmbH
In development of the new device was invested 286.6 billion Korean won or 252 million dollars. In total, South Korea plans to place five satellites with similar functionality in orbit. Kompsat - 3A, identical to Kompsat-3, launched on 26.03.2015. The KompSat-3 spacecraft consists of a payload-an AEISS (Advanced Earth Imaging Sensor System) camera and a satellite platform that takes it into space. The height of The KompSat-3 spacecraft is about 3.5 m with a diameter of 2.0 m in the withdrawal configuration. With the deployed solar panels and x-band antennas, the height and length are respectively about 4.7 and 6.9 m. the mass of the KompSat-3 spacecraft in the refueled state is about 1000 kg.
Technical characteristics of the spacecraft KompSat-3, 3A:
Name of the spacecraft; KompSat-3,3A
Country; South Korea
Developer; KARI, EADS Astrium
Operator; KARI
Launch vehicle; Rokot-KM
Launch date;KompSat-3 17.05.2012<br>KompSat-3A 26.03.2015
Orbit:<br> height, km<br> inclination, degree<br> circulation period, min<br> number of turns per day<br> time at the equator, hour;Solar-synchronous daytime<br>685<br>98,1<br>98.5<br>14.6<br>13:30
Platform:<br> shooting equipment<br> deflection angle, deg, deg;—<br>AEISS<br>45
Period of active existence, years; 4
Follow-up period, day; 3
Power, W ;1300
Size of spacecraft, m×m; 3.5×2.0
Mass of spacecraft, kg; 1000
According to the Ministry of science and technology of South Korea, the satellite will provide the opportunity to obtain accurate weather data, information on atmospheric fronts and weather over the ocean. The authorities also say that the device can be used for monitoring in case of natural disasters,as well as environmental monitoring.
Technical characteristics of onboard survey equipment
Name of spacecraft ;KompSat-3; KompSat-3A
Name of shooting equipment; MSC
Focal length, m; 8,6
Diameter of the main mirror, cm; 80
Relative aperture; 1:12
Spectral ranges, microns;Panchromatic 0.45-0.90<br>Blue 0.45-0.52<br>Green 0.52-0.60<br>Red 0.63-0.69<br>NIR 0.76-0.90
Pan element size, microns; 8,75
Number of PAN elements, microns; 17,5
The number of elements of MS, mcm; 6000
Terrain resolution;0,5<br>2,0<br>16,8;0,5<br>1,6<br>12
Data transfer rate, Mbit / sec;320
Memory capacity, Gbit; 64; 96
The main cases of using data obtained from the spacecraft KompSat-3, 3A:
creating and updating topographic maps and plans up to 1: 5,000 scale.
creation of digital elevation models (DEM) of high accuracy.
engineering surveys for the construction of infrastructure transportation and production of oil and gas.
implementation of forest management works, inventory and assessment of forests.
inventory of agricultural land, creation of land use plans.
creation of city plans and schemes of territorial planning of municipal districts.
inventory and monitoring of transport, energy and information communications.