• ICROS
• /
• v.8 no.2
• /
• pp.10-17
• /
• 2002

• Proceedings of the Korean Institute of Communication Sciences Conference
• /
• 1992.10a
• /
• pp.105-112
• /
• 1992

• Journal of Korean Electronics
• /
• v.2 no.3
• /
• pp.18-19
• /
• 1982

• Broadcasting and Media Magazine
• /
• v.7 no.1
• /
• pp.58-69
• /
• 2002

• Broadcasting and Media Magazine
• /
• v.7 no.1
• /
• pp.70-80
• /
• 2002

• The Korean Publising Journal, Monthly
• /
• s.330
• /
• pp.52-53
• /
• 2003

• Magazine of the Korea Concrete Institute
• /
• v.22 no.1
• /
• pp.71-77
• /
• 2010

• Information and Communications Magazine
• /
• v.19 no.4
• /
• pp.104-117
• /
• 2002

• Journal of Korean Institute of Fire Investigation
• /
• v.4 no.1
• /
• pp.50-54
• /
• 2004

• Aerospace Engineering and Technology
• /
• v.4 no.2
• /
• pp.60-64
• /
• 2005

STSAT-2 will demonstrate the scientific mission(acquisition of brightness temperature of the earth at 23.8 GHz and 37 GHz) and spacecraft technologies(laser ranging, frame-type satellite structure, Dual-head star tracker, CCD sun sensor, pulsed plasma thruster, etc.). In this paper STSAT-2 satellite system is described. It includes the definition of the system and the overview of payloads and BUS.