Results of high speed flight demonstration phase II

Masaaki Yanagihara, Yoshikazu Miyazawa, Takao Munenaga, Stéphanie Venel, Sylvain Guedron, Jean Claude Cretenet

研究成果: 会議への寄与タイプ学会誌査読

4 被引用数 (Scopus)

抄録

The High-Speed Flight Demonstration (HSFD) project is the latest in a series of flight experiments in a research program into reusable space transportation systems being conducted by Japan Aerospace Exploration Agency (JAXA). The project consists of two phases: Phase I to verify an approach and landing system for the terminal phase of the return flight of a winged re-entry vehicle, and Phase II to clarify the transonic aerodynamic characteristics of a winged re-entry vehicle. The first Phase II flight took place on July 1st, 2003 at the Esrange test site near Kiruna in Sweden, in collaboration with Centre National d'Etudes Spatiales of France (CNES). Although the experiment had to be discontinued when the demonstrator was damaged after its recovery system malfunctioned, aerodynamic characteristics data were obtained at Mach 0.8 and are being used to evaluate wind tunnel estimates and Computational Fluid Dynamics (CFD) predictions. Fully autonomous flight control technologies for the transonic speed region were also demonstrated. The results are expected to provide essential information for the development of future reusable space transportation systems.

本文言語英語
ページ8509-8516
ページ数8
出版ステータス出版済み - 12月 1 2004
イベントInternational Astronautical Federation - 55th International Astronautical Congress 2004 - Vancouver, カナダ
継続期間: 10月 4 200410月 8 2004

その他

その他International Astronautical Federation - 55th International Astronautical Congress 2004
国/地域カナダ
CityVancouver
Period10/4/0410/8/04

!!!All Science Journal Classification (ASJC) codes

  • 航空宇宙工学
  • 宇宙惑星科学

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