Title of article
Study on Low Density and Heat-resistant Ablative Coating
Author/Authors
ZHENG، نويسنده , , Tian-liang and ZOU، نويسنده , , Jing-cheng and YU، نويسنده , , Bo and WANG، نويسنده , , Yue-hong and ZHANG، نويسنده , , Hua، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2005
Pages
6
From page
372
To page
377
Abstract
Low bulk density expanding vermiculite is prepared, and the surface modification of hollow Al2O3-SiO2 microspheres and the composition of the low density ablative coating are studied. Organic silicon epoxy resin and phenolic aldehyde resin are applied as film forming matters to get a series of ablative coating having a density of 0.4-0.6 g/cm3. The performance of the low density ablative coating is evaluated by mechanical, thermodynamic and oxygen acetylene ablation tests, and the results are as follows, adhesion is in the range of 2.97-4.63 MPa, conductivity is no more than 0. 1 kcal/(m·h· °C), line ablation rate is no more than 0.30 mm/s, mass ablation rate is in the range of 0.11-0.18 mm/s.
Keywords
ablative coating , modification , Low density , Filler
Journal title
Chinese Journal of Aeronautics
Serial Year
2005
Journal title
Chinese Journal of Aeronautics
Record number
2264555
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