Design verification of H-2A auxiliary engine support structure and transonic wind tunnel test

Autor:	Kanda, Atsushi, Kai, Takashi, Suito, Takanobu, Nakamichi, Jiro
Jazyk:	japonština
Rok vydání:	2004
Předmět:	H-2A rocket transonic wind tunnel 遷音速風洞 transonic flight 空力負荷 風洞試験 超音速飛行 ロケットエンジン設計 supersonic flight auxiliary engine H-2Aロケット 補助エンジン rocket engine design wind tunnel test aerodynamic load 遷音速飛行
Zdroj:	宇宙航空研究開発機構特別資料: 第67回 風洞研究会議論文集 = JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 67th Meeting. :9-13
ISSN:	1349-113X 0047-4290
Popis:	NAL (National Aerospace Laboratory of Japan) cooperates with NASDA (National Space Development Agency of Japan) to verify the design of the H-2A Auxiliary Engine Support Structures that are located between SSBs of the H-2A launch vehicle No.2. It is very difficult to know beforehand fluctuating aerodynamic loads applied to actual support structures. This paper shows how to verify the design of support structures. Moreover, results of wind tunnel tests in NAL Transonic Wind Tunnel (TWT-1) are shown. 資料番号: AA0047429002 レポート番号: JAXA-SP-03-004
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=jairo_______::151212dbd27ad4cc6471633761283b30 http://id.nii.ac.jp/1696/00006580/ Zobrazit plný text záznamu