Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Tatsushi OHASHI"'
Publikováno v:
Journal of Fluid Science and Technology, Vol 13, Iss 3, Pp JFST0020-JFST0020 (2018)
An inflatable membrane reentry vehicle has been developed as one of the innovative reentry technologies. A suborbital reentry demonstration using a sounding rocket was carried out in 2012. Contrary to the result of a preliminary study, the vehicle al
Externí odkaz:
https://doaj.org/article/c4f1c86751224d2ea486d39518f6d681
Publikováno v:
The Proceedings of the Fluids engineering conference. 2018:OS9-12
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2c24d7bf54f9930cb0a478cb1f4acc11
https://doi.org/10.1299/jsmefed.2018.os9-12
https://doi.org/10.1299/jsmefed.2018.os9-12
Publikováno v:
Physics of fluids. 32(7):075114
Aerodynamic instability in the attitude of an inflatable re-entry vehicle in the subsonic regime has been observed during suborbital re-entry. This causes significant problems for aerodynamic decelerators using an inflatable aeroshell; thus, mitigati
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d9793d629f9e7fd8c392dc2a6f04c8fd
http://hdl.handle.net/2115/82107
http://hdl.handle.net/2115/82107
Publikováno v:
Journal of Fluid Science and Technology, Vol 13, Iss 3, Pp JFST0020-JFST0020 (2018)
An inflatable membrane reentry vehicle has been developed as one of the innovative reentry technologies. A suborbital reentry demonstration using a sounding rocket was carried out in 2012. Contrary to the result of a preliminary study, the vehicle al
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::39119a0673ad4d0bc3903d700f5c1f1b
https://www.jstage.jst.go.jp/article/jfst/13/3/13_2018jfst0020/_pdf/-char/en
https://www.jstage.jst.go.jp/article/jfst/13/3/13_2018jfst0020/_pdf/-char/en