TECHNICAL DEMONSTRATIONS FOR REUSABLE SOUNDING ROCKET SYSTEM

被引：0
|
作者：
Nonaka, Satoshi [1 ]
Ogawa, Hiroyuki [1 ]
Naruo, Yoshihiro [1 ]
Inatani, Yoshifumi [1 ]
机构：
[1] Japan Aerosp Explorat Agcy, Inst Space & Astronaut Sci, Chuo Ku, Sagamihara, Kanagawa 2525210, Japan
来源：
SPACE FOR OUR FUTURE | 2013年 / 146卷
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：
A fully reusable sounding rocket is proposed and conceptually designed in ISAS/JAXA. In phase A in the proposed project, technical demonstrations for key technologies to develop the reusable sounding rocket are planed as follows; 1) reusable engine development and repeated operations, 2) reusable insulation development for cryogenic tank, 3) aerodynamic design and model flight demonstration for returning flight, 4) cryogenic liquid propellant management demonstration, 5) landing gear development and 6) health management system construction. In this paper, the present system design of the reusable sounding rocket and technical demonstrations are summarized.
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页码：697 / 702
页数：6
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