Zobrazeno 1 - 3
of 3
pro vyhledávání: '"Seiyu Kayuta"'
Publikováno v:
JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 51:141-150
The staged combustion hybrid rocket is under development by our research group since 1999. This hybrid rocket engine consists of two combustion chambers. The primary combustion chamber is the fuel tank itself filled with granular solid fuels. The fue
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e1d950ea31dd7caca52524ac8da8cdc3
https://doi.org/10.2322/jjsass.51.141
https://doi.org/10.2322/jjsass.51.141
Autor:
Rikio Yokota, Nobuhiro Tanatsugu, Seiyu Kayuta, Masahiro Kohno, Harunori Nagata, Ryoziro Akiba
Publikováno v:
Journal of the Japan Society for Aeronautical and Space Sciences. 45:365-370
To overcome defects of conventional hybrid rocket motors such as poor mass ratio and low combustion efficiency, the authors propose a new idea of design. The point of this idea is that the motor uses ‘wet towel propellant’, in which liquid oxidiz
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::818d5af36be327bcb47dbf93d2f12f9d
https://doi.org/10.2322/jjsass1969.45.365
https://doi.org/10.2322/jjsass1969.45.365
Autor:
Seiyu Kayuta, Kuniaki Toyoda, Ted Mitsuteru Sugiki, Yoshinori Aoki, Atushi Hujii, Harunori Nagata, Ryojiro Akiba, Shinichirou Kurita
Publikováno v:
The Proceedings of Conference of Hokkaido Branch. :266-267
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::50240da5df3d7d22a6e08877d4f96424
https://doi.org/10.1299/jsmehokkaido.2001.41.266
https://doi.org/10.1299/jsmehokkaido.2001.41.266