Analytical evaluation of the solid rocket motor nozzle surface recession by the alumina-carbon reaction

Autor:	Matsukawa, Yutaka, Sato, Yutaka
Jazyk:	angličtina
Rok vydání:	2008
Předmět:	integumentary system graphite ロケットノズル 推進薬燃焼 rocket nozzle nozzle flow nozzle geometry 固体燃料ロケットエンジン 黒鉛 後退 propellant combustion アブレーション材料 solid propellant rocket engine aluminum oxide nozzle wall 酸化アルミニウム ノズル流 ノズル壁 ablative material recession 化学アブレーション ノズル形状 chemical ablation
Zdroj:	宇宙航空研究開発機構特別資料 = JAXA Special Publication: Proceedings of Lectures and Workshop International: Recent Advances in Multidisciplinary Technology and Modeling. :168-174
ISSN:	1349-113X
Popis:	A theoretical model describing the chemical ablation of a solid rocket motor nozzle ablator by the alumina-carbon reaction is presented. An application of it to a typical solid rocket motor with a graphite nozzle ablator indicates a large influence of the reaction on the nozzle surface recession. 資料番号: AA0063824017 レポート番号: JAXA-SP-07-008E
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=jairo_______::e3819afaadf4de8a2e5d82196facccad http://id.nii.ac.jp/1696/00005666/ Zobrazit plný text záznamu