Chinese Space Science and Technology
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Xing Lianqun (Beijing Institute of Spacecraft Systems Engineering)
Online:
Abstract: The paper describes one of the ablative thermal protection struc- tures of a returnable satellite,and discusses the ablation mechanism and the computation method of the FL composite material and siliconerubber, and compares the results with those of test.Finally the paper gives a conclu- sire idea.
Xing Lianqun (Beijing Institute of Spacecraft Systems Engineering). AN ENGINEERING COMPUTATION OF ABLATIVE THERMAL PROTECTION STRUCTURE OF RETURNABLE SATELLITE[J]. Chinese Space Science and Technology.
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URL: https://journal26.magtechjournal.com/kjkxjs/EN/
https://journal26.magtechjournal.com/kjkxjs/EN/Y1991/V11/I02/26
