DEVELOPMENT AND FLIGHT RESULT OF GUIDANCE AND CONTROL SYSTEM FOR ENHANCED EPSILON LAUNCH VEHICLE

被引:0
|
作者
Yamaguchi, Hiroyuki [1 ]
Morita, Yasuhiro [1 ]
Imoto, Takayuki [1 ]
Yamamoto, Takayuki [1 ]
Saiki, Takanao [1 ]
Ohtsuka, Hirohito [2 ]
Tanaka, Kensaku [2 ]
机构
[1] Japan Aerosp Explorat Agcy JAXA, 2-1-1 Sengen, Tsukuba, Ibaraki 3058505, Japan
[2] IHI Aerosp Co Ltd IA, 9000 Fujiki, Tomioka, Gunma 3702398, Japan
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The Epsilon launch vehicle, the newest version of Japan's solid propulsion rocket, made its maiden flight in September of 2013. The purpose of the Epsilon launch vehicle is to provide small satellites with responsive launching with low-cost, user-friendly and efficient launch system. The first flight was successfully finished, JAXA has been conducting intensive researches on a more powerful and lower cost version of Epsilon. In order to minimize technical risks and to keep up with demand of future payloads, JAXA plans to take a step-by-step approach toward Future Launch System. As the first upgrade toward Future Launch System, JAXA has started the development of the Enhanced Epsilon. This development is mainly the renewal of the second stage, and also includes each subsystem's improvement. This paper describes the development and flight result of the Enhanced Epsilon's Guidance and Control System.
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页码:233 / 241
页数:9
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