New thermal protection system using high-temperature carbon fibre-reinforced plastic sandwich panel
被引:36
作者:
Kubota, Yuki
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Japan Aerosp Explorat Agcy, 6-13-1 Osawa, Mitakashi, Tokyo 1810015, JapanJapan Aerosp Explorat Agcy, 6-13-1 Osawa, Mitakashi, Tokyo 1810015, Japan
Kubota, Yuki
[1
]
Miyamoto, Ousei
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机构:
Waseda Univ, Grad Sch Mech Engn, Shinjyuku Ku, 3-4-1 Okubo, Tokyo 1698555, JapanJapan Aerosp Explorat Agcy, 6-13-1 Osawa, Mitakashi, Tokyo 1810015, Japan
Miyamoto, Ousei
[2
]
Aoki, Takuya
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Japan Aerosp Explorat Agcy, 6-13-1 Osawa, Mitakashi, Tokyo 1810015, JapanJapan Aerosp Explorat Agcy, 6-13-1 Osawa, Mitakashi, Tokyo 1810015, Japan
Aoki, Takuya
[1
]
Ishida, Yuichi
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Japan Aerosp Explorat Agcy, 6-13-1 Osawa, Mitakashi, Tokyo 1810015, JapanJapan Aerosp Explorat Agcy, 6-13-1 Osawa, Mitakashi, Tokyo 1810015, Japan
Ishida, Yuichi
[1
]
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Ogasawara, Toshio
[3
]
Umezu, Shinjiro
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Waseda Univ, Grad Sch Mech Engn, Shinjyuku Ku, 3-4-1 Okubo, Tokyo 1698555, JapanJapan Aerosp Explorat Agcy, 6-13-1 Osawa, Mitakashi, Tokyo 1810015, Japan
Umezu, Shinjiro
[2
]
机构:
[1] Japan Aerosp Explorat Agcy, 6-13-1 Osawa, Mitakashi, Tokyo 1810015, Japan
[2] Waseda Univ, Grad Sch Mech Engn, Shinjyuku Ku, 3-4-1 Okubo, Tokyo 1698555, Japan
[3] Tokyo Univ Agr & Technol, Dept Mech Engn, 2-24-16 Koganeishi, Nakama, Tokyo 1848588, Japan
Herein, a new lightweight thermal protection system was proposed to reduce the weight of a re-entry capsule. The proposed system employs an ablator as a thermal protection material, and a high-temperature polyimide carbon fibre-reinforced plastic (CFRP) sandwich panel as a structure member. The sandwich panel was designed to exhibit high thermal insulation and good mechanical properties at high temperature, and simultaneously ensure that the ablator has low thickness. Three-point bending was carried out at a high temperature up to 300 degrees C to evaluate shear strength and flexural rigidity of the sandwich panel. Further, the proposed thermal protection system was examined using an arc-heated plasma wind tunnel to evaluate its thermal protection performance and thermal response. The shear strength and the flexural rigidity of this high-temperature structure were 76.8 and 86.9% of that at room temperature, respectively, when evaluated at 300 degrees C. The proposed system achieved more than 40% weight reduction while maintaining high thermal insulation and recession resistance.
机构:
NASA, Langley Res Ctr, Vehicle Anal Branch, Space Syst & Concepts Div, Hampton, VA 23681 USANASA, Langley Res Ctr, Vehicle Anal Branch, Space Syst & Concepts Div, Hampton, VA 23681 USA
Desai, PN
Mitcheltree, RA
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机构:NASA, Langley Res Ctr, Vehicle Anal Branch, Space Syst & Concepts Div, Hampton, VA 23681 USA
Mitcheltree, RA
Cheatwood, FM
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机构:NASA, Langley Res Ctr, Vehicle Anal Branch, Space Syst & Concepts Div, Hampton, VA 23681 USA
机构:
Japan Aerosp Explorat Agcy, Struct & Adv Composite Res Unit, 6-13-1 Ohsawa, Mitaka, Tokyo 1810015, JapanJapan Aerosp Explorat Agcy, Struct & Adv Composite Res Unit, 6-13-1 Ohsawa, Mitaka, Tokyo 1810015, Japan
Kubota, Yuki
Furuta, Takefumi
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机构:
Kaneka Corp, Frontier Mat Dev Labs, Tokyo, JapanJapan Aerosp Explorat Agcy, Struct & Adv Composite Res Unit, 6-13-1 Ohsawa, Mitaka, Tokyo 1810015, Japan
Furuta, Takefumi
Ishida, Yuichi
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Japan Aerosp Explorat Agcy, Struct & Adv Composite Res Unit, 6-13-1 Ohsawa, Mitaka, Tokyo 1810015, JapanJapan Aerosp Explorat Agcy, Struct & Adv Composite Res Unit, 6-13-1 Ohsawa, Mitaka, Tokyo 1810015, Japan
Ishida, Yuichi
Yokota, Rikio
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Kaneka Corp, Frontier Mat Dev Labs, Tokyo, JapanJapan Aerosp Explorat Agcy, Struct & Adv Composite Res Unit, 6-13-1 Ohsawa, Mitaka, Tokyo 1810015, Japan
Yokota, Rikio
Miyauchi, Masahiko
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机构:
Kaneka Amer Holding Inc, Kaneka US Mat Res Ctr, Pasadena, TX USAJapan Aerosp Explorat Agcy, Struct & Adv Composite Res Unit, 6-13-1 Ohsawa, Mitaka, Tokyo 1810015, Japan
Miyauchi, Masahiko
Aoki, Takuya
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机构:
Japan Aerosp Explorat Agcy, Struct & Adv Composite Res Unit, 6-13-1 Ohsawa, Mitaka, Tokyo 1810015, JapanJapan Aerosp Explorat Agcy, Struct & Adv Composite Res Unit, 6-13-1 Ohsawa, Mitaka, Tokyo 1810015, Japan
机构:
NASA, Langley Res Ctr, Vehicle Anal Branch, Space Syst & Concepts Div, Hampton, VA 23681 USANASA, Langley Res Ctr, Vehicle Anal Branch, Space Syst & Concepts Div, Hampton, VA 23681 USA
Desai, PN
Mitcheltree, RA
论文数: 0引用数: 0
h-index: 0
机构:NASA, Langley Res Ctr, Vehicle Anal Branch, Space Syst & Concepts Div, Hampton, VA 23681 USA
Mitcheltree, RA
Cheatwood, FM
论文数: 0引用数: 0
h-index: 0
机构:NASA, Langley Res Ctr, Vehicle Anal Branch, Space Syst & Concepts Div, Hampton, VA 23681 USA
机构:
Japan Aerosp Explorat Agcy, Struct & Adv Composite Res Unit, 6-13-1 Ohsawa, Mitaka, Tokyo 1810015, JapanJapan Aerosp Explorat Agcy, Struct & Adv Composite Res Unit, 6-13-1 Ohsawa, Mitaka, Tokyo 1810015, Japan
Kubota, Yuki
Furuta, Takefumi
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h-index: 0
机构:
Kaneka Corp, Frontier Mat Dev Labs, Tokyo, JapanJapan Aerosp Explorat Agcy, Struct & Adv Composite Res Unit, 6-13-1 Ohsawa, Mitaka, Tokyo 1810015, Japan
Furuta, Takefumi
Ishida, Yuichi
论文数: 0引用数: 0
h-index: 0
机构:
Japan Aerosp Explorat Agcy, Struct & Adv Composite Res Unit, 6-13-1 Ohsawa, Mitaka, Tokyo 1810015, JapanJapan Aerosp Explorat Agcy, Struct & Adv Composite Res Unit, 6-13-1 Ohsawa, Mitaka, Tokyo 1810015, Japan
Ishida, Yuichi
Yokota, Rikio
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h-index: 0
机构:
Kaneka Corp, Frontier Mat Dev Labs, Tokyo, JapanJapan Aerosp Explorat Agcy, Struct & Adv Composite Res Unit, 6-13-1 Ohsawa, Mitaka, Tokyo 1810015, Japan
Yokota, Rikio
Miyauchi, Masahiko
论文数: 0引用数: 0
h-index: 0
机构:
Kaneka Amer Holding Inc, Kaneka US Mat Res Ctr, Pasadena, TX USAJapan Aerosp Explorat Agcy, Struct & Adv Composite Res Unit, 6-13-1 Ohsawa, Mitaka, Tokyo 1810015, Japan
Miyauchi, Masahiko
Aoki, Takuya
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h-index: 0
机构:
Japan Aerosp Explorat Agcy, Struct & Adv Composite Res Unit, 6-13-1 Ohsawa, Mitaka, Tokyo 1810015, JapanJapan Aerosp Explorat Agcy, Struct & Adv Composite Res Unit, 6-13-1 Ohsawa, Mitaka, Tokyo 1810015, Japan