TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, SPACE TECHNOLOGY JAPAN
Online ISSN : 1347-3840
ISSN-L : 1347-3840
g) Space Transportation
Preliminary Design of Winged Experimental Rocket by University Consortium
Masashi WAKITAKoichi YONEMOTOTomoki AKIYAMAShigeru ASOYuji KOHSETSUHarunori NAGATA
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2009 年 7 巻 ists26 号 p. Tg_21-Tg_26

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The project of Winged Experimental Rocket described here is a proposal by the alliance of universities (University Consortium) expanding and integrating the research activities of reusable space transportation system performed by individual universities, and is the proposal that aims at flight proof of the results of advanced research conducted by the universities and JAXA using the university-centered experimental launch systems. This paper verifies the validity of the winged experimental rocket by surveying the technical issues that should be demonstrated and by estimating the airframe scale, weight and finally the total cost. The development schedule of this project was set to five years, where two airframes of different scales will be developed to minimize the risks. A 1.5-meter-long airframe will be first manufactured and conduct flight tests in the third year to verify the design issues. Then, a 2.5-meter-long airframe will be finally developed and conduct a complete flight demonstration of various research issues in the fifth year.

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© 2009 The Japan Society for Aeronautical and Space Sciences
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