Study of the Effects of Heat Load, Ablator Density and Backup Structure upon the Thermal Protection Performance of Heat Shield Systems Consisting of Phenolic Carbon Ablators
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- KATO Sumio
- University of the Ryukyus
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- MATSUDA Shoichi
- University of the Ryukyus
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- OKUYAMA Keiichi
- Kyushu Institute of Technology
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- GIBO Kenta
- Okinawa National College of Technology
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- OYA Hiroaki
- Kawasaki Heavy Industries, Ltd.
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- WATANABE Akihiro
- University of the Ryukyus
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- SHIMADA Naoyuki
- University of the Ryukyus
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- SAKAI Shunsuke
- University of the Ryukyus
説明
<p>The effects of heat load, ablator density, and backup structure, etc. upon the heat shield performance of the lightweight phenolic carbon ablators named LATS were investigated using a one-dimensional ablation analysis code. The ablator density was assumed to be from about 260 to 1000 kg/m3. Heat flux time histories of a rectangular pattern were assumed, where cases of constant heating duration time and constant accumulated heat load (up to 600 MJ/m2) were considered. The heating level was assumed to be from 1 to 10 MW/m2, which means that the ablator surface is in the region of diffusion control oxidation/sublimation. The materials of the backup wall are assumed to be aluminum, stainless steel and high density CFRP. Main findings are: (1) For a low heat flux q with the same heating duration time tq, the necessary thickness, with which the maximum back surface temperature equals to the pre-determined allowable temperature, is nearly constant as the density ρv changes. On the other hand, the necessary thickness increases largely when q is larger and ρv is smaller. The ablator necessary mass increases with the increase of ρv and q for the same tq. (2) When a backup wall is attached, the necessary thickness decreases and the necessary mass including the wall mass increases. (3) For a constant accumulated heat load, necessary thickness and mass decrease for a higher heat flux q especially when ρv is high. (4) A lower density ablator with a CFRP backup wall gives the lightest mass of the heat shield system for most of the parameter range among the three wall materials. (5) For a high heat flux, selection of a lower density ablator gives a larger necessary thickness.</p>
収録刊行物
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- TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 14 (ists30), Pe_95-Pe_104, 2016
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390282680298008960
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- NII論文ID
- 130005172209
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- ISSN
- 18840485
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- HANDLE
- 10228/00007258
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- 本文言語コード
- en
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- 資料種別
- conference paper
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- データソース種別
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- JaLC
- IRDB
- Crossref
- CiNii Articles
- OpenAIRE
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- 抄録ライセンスフラグ
- 使用不可