Analysis of Orbital Thermal Environment for Inclined-LEO Small Satellite

Jia Liu; Chao Lun Wang; Yun Ze Li

doi:10.4028/www.scientific.net/AMR.1016.446

Paper Titles

Improvement Design of the Insulation Structure of High Temperature Pneumatic Duct System of the Aircraft
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Design and Development of Vertical Takeoff and Horizontal Transition Mini Unmanned Aerial Vehicle
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Study on Serial MPPT Electrical Power System Stability for Space Application
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Analysis of Orbital Thermal Environment for Inclined-LEO Small Satellite
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State-Space Rotor Aeroelastic Modeling for Real-Time Helicopter Flight Simulation
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Flight Loads Analysis of a Maneuvering Transport Aircraft
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Effect of Reduced Frequency on Longitudinal Oscillatory Derivatives of an Airfoil Based on Wind Tunnel Data
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SOA-Cloud Computing Based Fast and Scalable Simulation Architecture for Advanced Flight Management System
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HomeAdvanced Materials ResearchAdvanced Materials Research Vol. 1016Analysis of Orbital Thermal Environment for...

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 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 of.

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Periodical:

Advanced Materials Research (Volume 1016)

Pages:

446-450

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.1016.446

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Online since:

August 2014

Authors:

Jia Liu*, Chao Lun Wang, Yun Ze Li

Keywords:

Inclined-LEO, Orbit β Angle, Orbital Thermal Environment, Small Satellite, β

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* - Corresponding Author

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