TY - GEN
T1 - Thermal control design and verification of BUAA-SAT
AU - Han, Jianbin
AU - Wang, Xinsheng
AU - Lee, Bo
AU - Zhou, Kaixing
AU - Ma, Haibo
AU - Dai, Yongchao
PY - 2012
Y1 - 2012
N2 - The BUAA-SAT is a micro-satellite mainly developed by graduate student of Beihang University with the purpose of space technology test and education. The satellite's volume is 300><300x500mm, with mass of 30kg and power of 11W. The thermal control design of the satellite uses some method such as ML1 blanket, thermal control coating, and some other passive thermal control method. A FEM thermal model was constructed in Ansys to get some theoretical result. Finally, the thermal balance test is described to verify the thermal design and the result of the thermal model.
AB - The BUAA-SAT is a micro-satellite mainly developed by graduate student of Beihang University with the purpose of space technology test and education. The satellite's volume is 300><300x500mm, with mass of 30kg and power of 11W. The thermal control design of the satellite uses some method such as ML1 blanket, thermal control coating, and some other passive thermal control method. A FEM thermal model was constructed in Ansys to get some theoretical result. Finally, the thermal balance test is described to verify the thermal design and the result of the thermal model.
UR - https://www.scopus.com/pages/publications/84883533914
M3 - 会议稿件
AN - SCOPUS:84883533914
SN - 9781622769797
T3 - Proceedings of the International Astronautical Congress, IAC
SP - 4534
EP - 4539
BT - 63rd International Astronautical Congress 2012, IAC 2012
T2 - 63rd International Astronautical Congress 2012, IAC 2012
Y2 - 1 October 2012 through 5 October 2012
ER -