@inproceedings{33ca50ccf0ce4ec2b1b8e5637558b26c,
title = "Analysis of orbital thermal environment for inclined-LEO small satellite",
abstract = "Spacecraft thermal design is a process of energy management in which environmental heating plays a major role. This paper is aimed at modeling and analysis of the orbital thermal environment by considering the external heat radiation, for the inclined-LEO cubed satellite with 3-axis stabilized (to Earth state).The result indicates that the analytical model simplifies the analysis of orbital thermal environment and the absolute value of β angle on inclined orbit can vary from 0 to a maximum which equals to the sum of orbit inclination and the maximum declination of the sun. Finally, for the inclined-LEO small satellite, the extreme thermal case should fully take account of the point ofβ *.",
keywords = "Inclined-LEO, Orbit β angle, Orbital thermal environment, Small satellite, β *",
author = "Jia Liu and Wang, \{Chao Lun\} and Li, \{Yun Ze\}",
year = "2014",
doi = "10.4028/www.scientific.net/AMR.1016.446",
language = "英语",
isbn = "9783038352235",
series = "Advanced Materials Research",
publisher = "Trans Tech Publications Ltd",
pages = "446--450",
booktitle = "Mechanical and Aerospace Engineering V",
address = "瑞士",
note = "5th International Conference on Mechanical and Aerospace Engineering, ICMAE 2014 ; Conference date: 18-07-2014 Through 19-07-2014",
}