Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Kaito Nakagawa"'
Publikováno v:
Scientific Reports, Vol 11, Iss 1, Pp 1-11 (2021)
Abstract Straintronics is a new concept to enhance electronic device performances by strain for next-generation information sensors and energy-saving technologies. The lattice deformation in graphene can modulate the thermal conductivity because phon
Externí odkaz:
https://doaj.org/article/0e3571d2d1614cae978855e687a055ec
Publikováno v:
Scientific Reports
Scientific Reports, Vol 11, Iss 1, Pp 1-11 (2021)
Scientific Reports, Vol 11, Iss 1, Pp 1-11 (2021)
Straintronics is a new concept to enhance electronic device performances by strain for next-generation information sensors and energy-saving technologies. The lattice deformation in graphene can modulate the thermal conductivity because phonons are t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::22091a63ba854c29e24025e5231819b3
https://pubmed.ncbi.nlm.nih.gov/34599219
https://pubmed.ncbi.nlm.nih.gov/34599219
Publikováno v:
Japanese Journal of Applied Physics. 56(6S1):06GN18-06GN18-8
We have fabricated needle-shaped emitters on a Si wafer by a MEMS process, and measured the voltage–current characteristics and the frequency dependence of a bipolar pulse voltage for ionic liquid electrospray thrusters, which can be mounted on nan
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::bcc0856814d1ace38a39d0dc1404b6bf
http://hdl.handle.net/10131/00011931
http://hdl.handle.net/10131/00011931
Autor:
Yoshinori Takao, Kaito Nakagawa
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN. 14:Pb_63-Pb_68
We have investigated the plasma production in a micro RF ion thruster, where the plasma source is 5.0 mm in radius and 10 mm in length. To find the optimum condition to generate the RF plasma in the wide range of frequency f = 1-1000 MHz and pressure
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::36de0cbd2f60ac6eff0ebc95650d3fbd
https://doi.org/10.2322/tastj.14.pb_63
https://doi.org/10.2322/tastj.14.pb_63
Autor:
Kaito NAKAGAWA, Yoshinori TAKAO
Publikováno v:
Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan; 2016, Vol. 14 Issue ists 30, p63-68, 6p