Author:
Gorodetsky M A,Mikhaylovsky K V,Reznik S V
Abstract
Abstract
A method for the integrated analysis and the determination of the composite construction parameters of a platform of the Earth remote sounding spacecraft, is proposed. The conditions of thermal load for a flight along a sun-synchronous orbit were analysed. The mathematical simulation of the operating conditions ensuring the effective operation of such satellites was performed. The method was tested with account of the input parameters of the «BelKA» satellite orbit. This method will be useful when selecting a working orbit for such satellites at the stage of technical proposals, since it includes determination of their orbital characteristics, as well as the heat flows onto the elements of their construction. The results of simulation of thermal regime of the composite structure options are presented.
Reference16 articles.
1. Properties of multilayer polymer composites based on non-woven material made of polyethylene terephthalate;Nelyub;Bulletin of Kazan Technological University,2017
2. Development of methods for determining and correcting the parameters of the working orbit of the Earth remote sensing spacecraft;Mikhailovsky;Bulletin of RUDN. Engineering research,2017
Cited by
1 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. The methods of designing an ultralight carbon fiber wing using parametrical modeling;XLIV ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration;2021