Thermal responses of a large nose cap model tested at SCIROCCO

Yoshiki Morino; Sebastiano Caristia

Thermal responses of a large nose cap model tested at SCIROCCO

Yoshiki Morino^*, Sebastiano Caristia

^*この研究の対応する著者

研究成果: Conference contribution

2 被引用数 (Scopus)

抄録

SCIROCCO, the largest plasma wind tunnel facility of the world, was used to test the full-scale geometrical model of the HYFLEX nose cap constructed of ceramic materials in order to evaluate the reentry heating simulation method on large structural elements. The temperature and pressure responses of the model surface were successfully measured and compared with the flight data and analytical calculations. Surface pressure responses were mostly as expected. Some interesting responses related to temperatures and heating rates were detected and are discussed in terms of catalytic recombination effects.

本文言語	English
ホスト出版物のタイトル	43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers
ページ	11609-11618
ページ数	10
出版ステータス	Published - 2005
外部発表	はい
イベント	43rd AIAA Aerospace Sciences Meeting and Exhibit - Reno, NV 継続期間: 2005 1月 10 → 2005 1月 13

Other

Other	43rd AIAA Aerospace Sciences Meeting and Exhibit
City	Reno, NV
Period	05/1/10 → 05/1/13

ASJC Scopus subject areas

工学（全般）

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引用スタイル

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title = "Thermal responses of a large nose cap model tested at SCIROCCO",

abstract = "SCIROCCO, the largest plasma wind tunnel facility of the world, was used to test the full-scale geometrical model of the HYFLEX nose cap constructed of ceramic materials in order to evaluate the reentry heating simulation method on large structural elements. The temperature and pressure responses of the model surface were successfully measured and compared with the flight data and analytical calculations. Surface pressure responses were mostly as expected. Some interesting responses related to temperatures and heating rates were detected and are discussed in terms of catalytic recombination effects.",

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AB - SCIROCCO, the largest plasma wind tunnel facility of the world, was used to test the full-scale geometrical model of the HYFLEX nose cap constructed of ceramic materials in order to evaluate the reentry heating simulation method on large structural elements. The temperature and pressure responses of the model surface were successfully measured and compared with the flight data and analytical calculations. Surface pressure responses were mostly as expected. Some interesting responses related to temperatures and heating rates were detected and are discussed in terms of catalytic recombination effects.

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BT - 43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers

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Y2 - 10 January 2005 through 13 January 2005

ER -

Thermal responses of a large nose cap model tested at SCIROCCO

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