The satellite experiences the launch environment such as vibration, acceleration, shock induced by rocket and the orbit environment such as high vacuum, no gravity, high temperature and cryogenic. Therefore, the satellite should be designed and manufactured to endure such environments. Also, special care must be taken on the assembly of parts and subsystem. Finally, we describe the environment test of microsatellite to ensure the reliable operation during launch period as well as in-orbit operation
The telecommand system of KITSAT micorsatellite receives commands from ground stations or on-board c...
The costs involved in building and launching standard big satellites are very high. Due to the minia...
This thesis describes the development of a working thermal model of the Naval Postgraduate School's ...
SaTReC has developed and operated two micro-satellites, KITSAT-1 and 2 successfully. Since middle of...
This study is based upon the thermal modeling, analysis and operational results of KITSAT-1 and KITS...
The results of space radiation experiments carried out on board the first two Korean technology demo...
Since mid-2014, the fully integrated small satellite Flying Laptop is in the system testing phase at...
OUFTI-1’s test campaigns were divided into two phases. The goal of Phase 1 is to demonstrate that th...
This paper is to report the result of the first Korean satellite, KITSAT-OSCAR 23 (KITSAT-1) and to ...
This paper presents the basic research for establishing the qualification test (QT) level a unit has...
Satellite Technology Research Center(SaTReC) of Korean Advanced Institute of Science and Technology(...
A versatile test facility has been designed and built to study space environments effects on small s...
Students from the Indian Institute of Technology Bombay (IITB) are currently in the process of build...
The Satellite Technology Research Center (SaTReC) has successfully developed and operated three micr...
Demand of an environment test facility suitable for micro/nano satellites has increased as the numbe...
The telecommand system of KITSAT micorsatellite receives commands from ground stations or on-board c...
The costs involved in building and launching standard big satellites are very high. Due to the minia...
This thesis describes the development of a working thermal model of the Naval Postgraduate School's ...
SaTReC has developed and operated two micro-satellites, KITSAT-1 and 2 successfully. Since middle of...
This study is based upon the thermal modeling, analysis and operational results of KITSAT-1 and KITS...
The results of space radiation experiments carried out on board the first two Korean technology demo...
Since mid-2014, the fully integrated small satellite Flying Laptop is in the system testing phase at...
OUFTI-1’s test campaigns were divided into two phases. The goal of Phase 1 is to demonstrate that th...
This paper is to report the result of the first Korean satellite, KITSAT-OSCAR 23 (KITSAT-1) and to ...
This paper presents the basic research for establishing the qualification test (QT) level a unit has...
Satellite Technology Research Center(SaTReC) of Korean Advanced Institute of Science and Technology(...
A versatile test facility has been designed and built to study space environments effects on small s...
Students from the Indian Institute of Technology Bombay (IITB) are currently in the process of build...
The Satellite Technology Research Center (SaTReC) has successfully developed and operated three micr...
Demand of an environment test facility suitable for micro/nano satellites has increased as the numbe...
The telecommand system of KITSAT micorsatellite receives commands from ground stations or on-board c...
The costs involved in building and launching standard big satellites are very high. Due to the minia...
This thesis describes the development of a working thermal model of the Naval Postgraduate School's ...