Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Misuzu Matsuoka"'
Autor:
Isai Fajardo, Aleksander A. Lidtke, Sidi Ahmed Bendoukha, Jesus Gonzalez-Llorente, Rafael Rodríguez, Rigoberto Morales, Dmytro Faizullin, Misuzu Matsuoka, Naoya Urakami, Ryo Kawauchi, Masayuki Miyazaki, Naofumi Yamagata, Ken Hatanaka, Farhan Abdullah, Juan J. Rojas, Mohamed Elhady Keshk, Kiruki Cosmas, Tuguldur Ulambayar, Premkumar Saganti, Doug Holland, Tsvetan Dachev, Sean Tuttle, Roger Dudziak, Kei-ichi Okuyama
Publikováno v:
Aerospace, Vol 6, Iss 10, p 108 (2019)
Ten-Koh is a 23.5 kg, low-cost satellite developed to conduct space environment effects research in low-Earth orbit (LEO). Ten-Koh was developed primarily by students of the Kyushu Institute of Technology (Kyutech) and launched on 29 October 2018 on-
Externí odkaz:
https://doaj.org/article/77470aa6d66f46fdab082c062bdb275e
Publikováno v:
International Journal of Research -GRANTHAALAYAH. 6:121-131
Micro satellites must survive severe mechanical conditions during their launch phase. One design requirement for rockets is the stiffness requirement, i.e. the natural frequencies requirement. In the early stages of satellite development, presumption
Autor:
Sean Tuttle, Doug Holland, Misuzu Matsuoka, Tsvetan Dachev, Rafael Rodríguez, Masayuki Miyazaki, Naoya Urakami, Roger Dudziak, Tuguldur Ulambayar, Ken Hatanaka, Aleksander A. Lidtke, Jesus Gonzalez-Llorente, Kei Ichi Okuyama, Naofumi Yamagata, Mohamed Elhady Keshk, Juan José Rojas, Rigoberto Morales, Premkumar B. Saganti, Kiruki Cosmas, Ryo Kawauchi, Dmytro Faizullin, Farhan Abdullah, Sidi Ahmed Bendoukha, Isai Fajardo
Publikováno v:
Aerospace, Vol 6, Iss 10, p 108 (2019)
Aerospace
Volume 6
Issue 10
Aerospace
Volume 6
Issue 10
Ten-Koh is a 23.5 kg, low-cost satellite developed to conduct space environment effects research in low-Earth orbit (LEO). Ten-Koh was developed primarily by students of the Kyushu Institute of Technology (Kyutech) and launched on 29 October 2018 on-
Micro satellites must survive severe mechanical conditions during their launch phase. One design requirement for rockets is the stiffness requirement, i.e. the natural frequencies requirement. In the early stages of satellite development, presumption
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e4a15b000e934dfd8c17757ef8a4067b
Autor:
Fajardo, Isai, Lidtke, Aleksander A., Bendoukha, Sidi Ahmed, Gonzalez-Llorente, Jesus, Rodríguez, Rafael, Morales, Rigoberto, Faizullin, Dmytro, Misuzu Matsuoka, Naoya Urakami, Ryo Kawauchi, Masayuki Miyazaki, Naofumi Yamagata, Ken Hatanaka, Abdullah, Farhan, Rojas, Juan J., Keshk, Mohamed Elhady, Cosmas, Kiruki, Ulambayar, Tuguldur, Saganti, Premkumar, Holland, Doug
Publikováno v:
Romanian Journal of Morphology & Embryology; 2019, Vol. 60 Issue 2, p1-38, 38p