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- FURUTA Toshiyasu
- 航空宇宙技術研究所
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- GODAI Tomifumi
- 航空宇宙技術研究所
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- TOYOHARA Tsunehiko
- 航空宇宙技術研究所
Bibliographic Information
- Other Title
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- 耐熱複合材の研究
- タイネツ フクゴウザイ ノ ケンキュウ
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Abstract
Ablative behavior of cloths of impregnated carbon, silica and ceramic with phenolic resin, was investigated experimentally by oxygen-acetylene torch testings and aluminized solid propellant motor firing.<BR>The heat transfer coefficient on specimens under torch testings and motor firing test was 0.05 to 0.2 and 0.5 to 1.6kcal/mm2sec°C, respectively.<BR>From the data obtained by torch testing and sub-scale solid motor firing test, a combination of carbon GF-20/phenolic 5900 was chosen as the throat material of the 6-in solid motor.<BR>The ablative characteristic of the composite material was obtained successfully by firing.<BR>Of interest was the fact there was no variation in the throat diameter ofter firing. It was shown that the calculated temperature history agreed well with experiment, and that, due to ablation, the equivalent heat transfer rate decreased to 4 % of heat transfer rate without ablation.
Journal
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- Aeronautical and Space Sciences Japan
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Aeronautical and Space Sciences Japan 17 (182), 126-128, 1969
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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Details 詳細情報について
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- CRID
- 1390282679481933056
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- NII Article ID
- 130003782148
- 40018294699
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- NII Book ID
- AN00189072
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- ISSN
- 24241369
- 00214663
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- NDL BIB ID
- 8378291
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- Text Lang
- ja
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- Data Source
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed