期刊
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING
卷 41, 期 10, 页码 1483-1490出版社
ELSEVIER SCI LTD
DOI: 10.1016/j.compositesa.2010.06.010
关键词
Foams; High temperature properties; Thermal analysis; Cure, heat treatment
Thermal protection systems (TPS) are designed to protect re-entry space vehicles from the severe heating encountered during hypersonic flight through a planet's or the earth's atmosphere. A carbon-phenolic ablative TPS was developed, manufactured and tested with the aim of fulfilling the thermal and mechanical requirements corresponding to the actual loads experienced by a vehicle during a moon-earth re-entry. Experimental activities were carried out on two different composite systems (a resole resin coupled with a graphitic felt and a graphitic foam), and were aimed to the optimization of the manufacturing procedure and to the characterization of the mechanical behaviour and of the insulation performance of the fabricated composites. (c) 2010 Elsevier Ltd. All rights reserved.
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