Zobrazeno 1 - 10
of 26
pro vyhledávání: '"Shinjae Kang"'
Autor:
Shinjae Kang, Sejin Kwon
Publikováno v:
Materials, Vol 14, Iss 11, p 2828 (2021)
Spacecraft have monopropellant thruster systems for attitude control in the vacuum of space. Hydroxylamine nitrate is a green propellant that has high performance and low toxicity. Owing to the high adiabatic decomposition temperature of the hydroxyl
Externí odkaz:
https://doaj.org/article/bb38095e8d0e4877ae75cce11aa5153e
Autor:
Shinjae Kang
Publikováno v:
Acta Astronautica. 205:47-56
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::60cd6b68fe217d5c7cd56bdd0afee0b3
https://doi.org/10.1016/j.actaastro.2023.01.029
https://doi.org/10.1016/j.actaastro.2023.01.029
Autor:
Shinjae Kang, Sanggwan Oh
Publikováno v:
Journal of the Brazilian Society of Mechanical Sciences and Engineering. 45
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e94e5ad769714dde7f9e57322b0d7bc8
https://doi.org/10.1007/s40430-023-04038-8
https://doi.org/10.1007/s40430-023-04038-8
Publikováno v:
CEAS Space Journal. 13:189-196
In this study, a manganese oxide lanthanum-doped alumina (MnOx/La/Al2O3) catalyst was employed for application in a 95 wt.% hydrogen peroxide thruster. By employing 95 wt.% hydrogen peroxide rather than the conventional 87.5 wt.% hydrogen peroxide, s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c4049a65e555393d47921a09f98ca5a9
https://doi.org/10.1007/s12567-020-00334-4
https://doi.org/10.1007/s12567-020-00334-4
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 47:335-343
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ae3e345a8232696408f13ce76aa0fb50
https://doi.org/10.5139/jksas.2019.47.5.335
https://doi.org/10.5139/jksas.2019.47.5.335
Autor:
Min-Seok Moon, Joonhyuk Song, Kwang-Seok Kim, Je-Ha Oh, Sung-Mo Yang, ShinJae Kang, MyeongHan Yoo
Publikováno v:
Robotics and Computer-Integrated Manufacturing. 55:154-159
Recently, interest in light-weight vehicle research is spreading swiftly across the globe. This is part of efforts to reduce CO2 emissions in many countries of the world, including developed countries. Magnesium alloys represent light-weight, metalli
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::248422b2da81158fa6fd7b8aea2e9548
https://doi.org/10.1016/j.rcim.2018.01.004
https://doi.org/10.1016/j.rcim.2018.01.004
Autor:
Sejin Kwon, Shinjae Kang
Publikováno v:
Materials
Volume 14
Issue 11
Materials, Vol 14, Iss 2828, p 2828 (2021)
Volume 14
Issue 11
Materials, Vol 14, Iss 2828, p 2828 (2021)
Spacecraft have monopropellant thruster systems for attitude control in the vacuum of space. Hydroxylamine nitrate is a green propellant that has high performance and low toxicity. Owing to the high adiabatic decomposition temperature of the hydroxyl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7c3a065063872f5f66832d07556e493d
http://europepmc.org/articles/PMC8199400
http://europepmc.org/articles/PMC8199400
Publikováno v:
Fibers and Polymers. 18:1609-1613
Long fiber thermoplastics (LFT) ribs co-molded with woven glass fabric prepregs were considered to design an automotive side impact beam (SIB). The LFT ribs were designed to locate at the center of the continous fiber reinfoced SIB. The woven fabric
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bd92edaf33417ae9530684805920238f
https://doi.org/10.1007/s12221-017-6927-z
https://doi.org/10.1007/s12221-017-6927-z
Publikováno v:
Acta Astronautica. 130:75-83
The decomposition process of hydrogen peroxide can be applied to a bipropellant thruster, as well as to monopropellant thruster. To provide a framework for the optimal design of the injector and catalyst bed depending on a type of thruster, this rese
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::85bd33d0856a3f9beb245e6938a1a83c
https://doi.org/10.1016/j.actaastro.2016.10.023
https://doi.org/10.1016/j.actaastro.2016.10.023
Publikováno v:
2018 Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::221c7adc970610c0202b337145c8b977
https://doi.org/10.2514/6.2018-4526.c1
https://doi.org/10.2514/6.2018-4526.c1