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
Autor:
Hirohide Ikeda, Keigo Hatai
Publikováno v:
JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 67:174-180
Publikováno v:
AIAA Propulsion and Energy 2019 Forum.
Publikováno v:
Transactions of the JSME (in Japanese). 82:15-00667
Publikováno v:
2018 Joint Propulsion Conference.
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
Publikováno v:
The Proceedings of the Materials and Mechanics Conference. 2015:GS0502-29
Publikováno v:
Transactions of the JSME (in Japanese). 81:15-00243