Zobrazeno 1 - 10
of 14
pro vyhledávání: '"Bum-Seok Hyun"'
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 46:1028-1036
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::47b2dd6cd3b09d6be668b08575671c19
https://doi.org/10.5139/jksas.2018.46.12.1028
https://doi.org/10.5139/jksas.2018.46.12.1028
Autor:
Su-Young Chang, Bum-Seok Hyun, Hyeong Yul Cheon, Jang-Joon Lee, Taig Young Kim, Jung-Hoon Kim, Hang-Pal Hua
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 46:338-344
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6dcec56e78a16ae3ca7b358c7fdc2ab8
https://doi.org/10.5139/jksas.2018.46.4.338
https://doi.org/10.5139/jksas.2018.46.4.338
Publikováno v:
Aerospace Science and Technology. 54:330-339
This paper deals with alternative multi-functional structures by using grid-stiffened composite panel with excellent bending stiffness and lightweight characteristics. The grid-stiffened multi-functional structure can provide an array of available ro
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d3407afc4fecb2beea683d626451caa2
https://doi.org/10.1016/j.ast.2016.05.002
https://doi.org/10.1016/j.ast.2016.05.002
Autor:
Hyeong Yul Cheon, Young Bae Seo, Taig Young Kim, Jung-gi Seo, Bum-Seok Hyun, Yoon Sub Shin, Tae Su Kim
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 44:373-379
The thermal control device for the periodic working component combined solid-liquid phase change material (PCM) with heat pipes is designed and numerically studied. Due to high latent heat and retaining constant temperature during melting process the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4490b3ea4f870b170d030a1280a7e564
https://doi.org/10.5139/jksas.2016.44.4.373
https://doi.org/10.5139/jksas.2016.44.4.373
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 42:1013-1019
'( ) * +&! * , % &&!-*+ % ./0* &&&!/0% )*$1% &&&( ( 2%%&&&% ( +% 34%5( 5($6 %% ! %(7 $0 %5 58 9% : 0& %( 9( 5% : * % 3 5 % 5%( '%5 $ 0&& %( % :(5%;%:%( 5 : * %&&& $ $ :( %$$ % : *+% 5($$0: * % = 55( >%:*>: * % = '% +($-*33% 4(:: '-4 '%%$%5 5($+ *$% 2
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cb52b1bbc48e355747c5a64f7ed19317
https://doi.org/10.5139/jksas.2014.42.12.1013
https://doi.org/10.5139/jksas.2014.42.12.1013
Publikováno v:
Aerospace Science and Technology. 27:10-16
A new spacecraft thermal control hardware composed of two parallel channels working for heat pipe (HP) and solid–liquid phase change material (PCM), respectively, is suggested for the high heat dissipating component which works intermittently with
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ce0dd8eb95970e4a3e6ee041165b8e38
https://doi.org/10.1016/j.ast.2012.05.007
https://doi.org/10.1016/j.ast.2012.05.007
Autor:
Ju-Hun Rhee, Taig-Young Kim, Hyun-Suk Seo, Tae-Seong Jang, Bum-Seok Hyun, Young-Bae Seo, Won-Seock Kim, Jang-Joon Lee
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 40:157-164
The design strategy of the multi-functional structure is that the electrical components and the circuits are directly put on their supporting structural panel in which the radiation shields and the thermal control functions are integrated. Applying t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cbb32c9790e1196d059215edb5e6eeaf
https://doi.org/10.5139/jksas.2012.40.2.157
https://doi.org/10.5139/jksas.2012.40.2.157
Autor:
Ju-Hun Rhee, Tae-Seong Jang, Won-Seock Kim, Im-Soo Kim, Eun-Sup Sim, Sang-Kon Lee, Hyun-Suk Seo, Jae Hyuk Lim, Bum-Seok Hyun, Do-Soon Hwang, Eun-Soo Han, Hee-Keun Cho
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 39:526-534
The MFS (Mlti-Functional Structure) concept, which integrates the electronics, thermal control and structure into a single packaging system, has been developed and applied to reduce the volume and weight of the satellite. Therefore, this MFS can elim
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e1a90fb241722afecaa28e1e97332103
https://doi.org/10.5139/jksas.2011.39.6.526
https://doi.org/10.5139/jksas.2011.39.6.526
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 38:1087-1093
The satellite thermal control H/W composed of two parallel channels working for heat pipe (HP) and phase change material (PCM) is suggested for the high heat dissipating component which works intermittently with short duty. In a limited point of view
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f450f35d26e3d742cdbfdac3ee298d1e
https://doi.org/10.5139/jksas.2010.38.11.1087
https://doi.org/10.5139/jksas.2010.38.11.1087
Publikováno v:
Journal of the Korean Society for Aeronautical Space Science. 37:916-922
Because thermal design of satellite carrying out mission in space is performed by thermal analysis result using thermal mathematical model, accuracy of thermal mathematical model is important and it can be improved by model correlation. Correlation s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0bdc8df5cd51e5f7f6ef674d3e744433
https://doi.org/10.5139/jksas.2009.37.9.916
https://doi.org/10.5139/jksas.2009.37.9.916