Zobrazeno 1 - 10
of 20
pro vyhledávání: '"Hirohide Ikeda"'
Publikováno v:
Nihon Kikai Gakkai ronbunshu, Vol 82, Iss 835, Pp 15-00667-15-00667 (2016)
Creep - fatigue analyses based on the concept of continuum damage mechanics were conducted for the combustion chamber used in a satellite's bipropellant thruster. The previously identified models and material parameters for the niobium alloy (C103) w
Externí odkaz:
https://doaj.org/article/c45ea6a4c7034a7b90ee28024d0218fa
Publikováno v:
Nihon Kikai Gakkai ronbunshu, Vol 81, Iss 829, Pp 15-00243-15-00243 (2015)
The elasto-plastic constitutive equation based on the concept of continuum damage mechanics was formulated for the niobium alloy (C103) which is used as a chamber material in a satellite's thruster. The existing theory was extended to deal with the c
Externí odkaz:
https://doaj.org/article/b0aa46fdd89542edaf8a34688a52a251
Autor:
Taiichi Nagata, Hirohide Ikeda
Publikováno v:
JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 69:105-112
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fe7c8edd2b4e3b2789858e93961ed829
https://doi.org/10.2322/jjsass.69.105
https://doi.org/10.2322/jjsass.69.105
Autor:
Hirohide Ikeda, Keigo Hatai
Publikováno v:
JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 67:174-180
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::64c4dbccc732264d57429ad5d15cdb9a
https://doi.org/10.2322/jjsass.67.174
https://doi.org/10.2322/jjsass.67.174
Publikováno v:
AIAA Propulsion and Energy 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5a3472437e31ada943c10ada6104f580
https://doi.org/10.2514/6.2019-4427
https://doi.org/10.2514/6.2019-4427
Publikováno v:
2018 Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1deaea7160352008aadee95a254d303d
https://doi.org/10.2514/6.2018-4753
https://doi.org/10.2514/6.2018-4753
Autor:
Hirohide Ikeda, Yuji Kawabata, Tadashi Masuoka, Taiichi Nagata, Yasushi Saito, Hideshi Kagawa, Daisuke Ito
Publikováno v:
Physics Procedia. 69:577-582
Most mono-propellant thruster technologies were developed in the 1960s. Those basic principles and fundamental mechanisms, such as the catalyst and propellant, are still in use without major technical innovation. However, much remains to be clarified
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::696fa3638305bec0e9c2c596066d74c2
https://doi.org/10.1016/j.phpro.2015.07.082
https://doi.org/10.1016/j.phpro.2015.07.082
Publikováno v:
The Proceedings of the Materials and Mechanics Conference. 2015:GS0502-29
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bff05f8953bd9a1de3069da42799d8c3
https://doi.org/10.1299/jsmemm.2015._gs0502-29
https://doi.org/10.1299/jsmemm.2015._gs0502-29
Publikováno v:
JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 63:225-231
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0b749d7c1a1c077304948e1242ae8f59
https://doi.org/10.2322/jjsass.63.225
https://doi.org/10.2322/jjsass.63.225
Autor:
Tomohiro Maruko, Hideyuki Murakami, Masahiro Sasaki, Yuichi Iwamoto, Tomoaki Miyazawa, Go Fujii, Hirohide Ikeda, Hideyuki Kobayashi, Kazuya Shimoda
Publikováno v:
53rd AIAA/SAE/ASEE Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::51b95f62da196ffbcfe3bd04fce4e7a8
https://doi.org/10.2514/6.2017-5013
https://doi.org/10.2514/6.2017-5013