An overview of the high speed flight demonstration project

Wataru Sarae, Takeshi Nishizawa, Masakazu Sagisaka, Toshio Akimoto, Yoshikazu Miyazawa, Masaaki Yanagihara, Stéphanie Venel, Sylvain Guedron, Jean Claude Cretenet

研究成果: Contribution to conferencePaper査読

2 被引用数 (Scopus)

抄録

An overview of flight experiments of the High Speed Flight Demonstration Project is presented. The project consists of two phases: Phases I and II. The Phase I flight experiment was conducted in Christmas Island, Republic of Kiribati from October to December 2002. Through three flights, we have demonstrated the vehicle's ability to fly a steep approach path (up to 25 degrees), which is characteristic of return flights of winged reentry vehicles, and have accumulated autonomous flight technologies needed for unmanned vehicles, including take-off and landing. A Flight experiment of Phase II was conducted at Esrange test site near Kiruna in Sweden from June to July 2003 in collaboration with Centre National d'Etudes Spatiales of France (CNES). Using the flight data, the vehicle's aerodynamic characteristics at a constant Mach number (0.8) over a wide range of angles of attack were estimated, and fully autonomous flight control technologies were demonstrated.

本文言語英語
ページ1895-1905
ページ数11
出版ステータス出版済み - 12 1 2003
イベント54th International Astronautical Congress of the International Astronautical Federation (IAF), the International Academy of Astronautics and the International Institute of Space Law - Bremen, ドイツ
継続期間: 9 29 200310 3 2003

その他

その他54th International Astronautical Congress of the International Astronautical Federation (IAF), the International Academy of Astronautics and the International Institute of Space Law
国/地域ドイツ
CityBremen
Period9/29/0310/3/03

All Science Journal Classification (ASJC) codes

  • 工学(全般)

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