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ANALYSIS OF DEPLOYMENT MOTION OF SATELLITE SOLAR WING

Chen Liemin (Beijing Institute of Spacecraft Systems Engineering)   

  • Published:1992-04-25

Abstract: Solar wing is the main component of various applied satellites. The analysis of its deployment motion on orbit plays an important role in satellite design.This paper presents a simple and rapid calculation method which is suitable for engineering application,

Key words: Solar sail, Deployment, Calculation method, Satellite