Chinese Space Science and Technology
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Li XiLun (Beijing Institute of Spacecraft Systems Engineering)
Online:
Abstract: This paper discusses the problem of aerodynamics heat of non-fairinged satellite.The method of heat-inertia in launching phase,is usedin thermal control design.The theoretical data,test data and flight data are identical with eachother.It shows that the design is very successful.
Li XiLun (Beijing Institute of Spacecraft Systems Engineering). THERMAL CONTROL DESIGN OF RETURNABLE SATELLITE IN LAUNCHING PHASE[J]. Chinese Space Science and Technology.
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https://journal26.magtechjournal.com/kjkxjs/EN/Y1991/V11/I04/67
