Attitude control, with 0.1 to 0.5 resolution and maximum 45 tilt about the roll axis, will be provided by momentum wheels, magnetic torquers, and thrusters. Propulsion system, to be used for orbit and attitude maneuvers, will use hydrazine as the propellant. It will have 50 kg capacity and will consist of six 5 Newton thrusters. Pegasus XL, Taurus, and LLV have been mentioned as candidate launchers. Some of the other participating universities include the Seoul National University, Yonsei University, and Inha University.
Industrial participation is as follows.
Korean Air and Duwon are in charge of structures and thermal analysis of structures. Daewoo is responsible for the attitude control system. Halla and Hanwha are developing the propulsion system. Hyundai is in charge of the power supply system. Samsung is responsible for the remote sensing system.