Zobrazeno 1 - 10
of 54
pro vyhledávání: '"Ryojiro MINATO"'
Publikováno v:
Propulsion and Power Research, Vol 11, Iss 4, Pp 444-456 (2022)
The main interest in the current study focuses on the possibility of overspeeding for the gas-generator cycle air turbo ramjet (GG-ATR) engine. The authors developed the air turbo ramjet engine and investigated its compressor performance. Based on th
Externí odkaz:
https://doaj.org/article/c740cd31959b43dbad89050c7235d035
Autor:
Ryojiro Minato
Publikováno v:
Propulsion and Power Research, Vol 11, Iss 3, Pp 311-324 (2022)
The present study proposes ethanol-nitromethane mixture as a safe, storable, and low toxic monopropellant for a gas generator cycle air turbo ramjet engine and evaluates its propulsion performance. The present study proposes that nitromethane is mixe
Externí odkaz:
https://doaj.org/article/e9dddd1f656944e396e39e23c9e2c96a
Autor:
Ryojiro Minato1 r-minato@mmm.muroran-it.ac.jp, Shigeru Tanaka2
Publikováno v:
Science & Technology of Energetic Materials. 2022, Vol. 83 Issue 4, p111-116. 6p.
Autor:
Daisuke Nakata, Ryojiro Minato, Hiromitsu Yagihashi, Masaharu Uchiumi, Inaho Yoshikawa, Koki Arimatsu
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN. 19:217-223
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::22595851f3223b1477e85fc7e7e794a9
https://doi.org/10.2322/tastj.19.217
https://doi.org/10.2322/tastj.19.217
Autor:
Ryojiro Minato
Publikováno v:
Aerospace Science and Technology. 91:337-356
The present study investigates the feasibility of alcohol fuels for a Gas Generator cycle Air Turbo Ramjet (GG-ATR) Engine in comparison with alkane fuels. The alkane and alcohol fuels in the present study range from C1 species (CH4 and CH3OH) to C4
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::35e58c2b3d66359d8c2b38caffb13e1c
https://doi.org/10.1016/j.ast.2019.05.023
https://doi.org/10.1016/j.ast.2019.05.023
Publikováno v:
The Proceedings of the Fluids engineering conference. 2018:OS8-15
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c5592f1c0484855f6ceb39f29cb347e7
https://doi.org/10.1299/jsmefed.2018.os8-15
https://doi.org/10.1299/jsmefed.2018.os8-15
Autor:
Naoki SOTA, Ryoji IMAI, Aoki ANADA, Taisei YAMAZAKI, Masaharu UCHIUMI, Daisuke NAKATA, Ryojiro MINATO
Publikováno v:
International Journal of Microgravity Science & Application; 2022, Vol. 39 Issue 1, p1-10, 10p
The Minimum Flow Rate of Liquid-Oxygen When Considering a Throttling of a Gas Generator Cycle Engine
Autor:
Inaho Yoshikawa, Daisuke Nakata, Masaharu Uchiumi, Ryojiro Minato, Koki Arimatsu, Hiromitsu Yagihashi
Publikováno v:
Volume 3A: Fluid Applications and Systems.
Currently in development at Muroran Institute of Technology, a small gas-generator-cycle air turbo ramjet engine (GG-ATR) for a supersonic unmanned aerial vehicle requiring deep throttling uses liquid oxygen/ethanol as a propellant. However, it is di
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c5e0f1953b909dd44242df8aaff07c83
https://doi.org/10.1115/ajkfluids2019-5621
https://doi.org/10.1115/ajkfluids2019-5621
Autor:
Ryojiro Minato
Publikováno v:
Aerospace Science and Technology. 50:161-172
Performance analyses of Gas Generator cycle Air Turbo Ramjet (GG-ATR) engine are conducted to investigate the feasibility of ethanol fuel, as comparing Liquefied Hydrogen (LH2), Liquefied Natural Gas (LNG), and n-C12H26. Liquefied Oxygen (LOX) is con
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4805efdbcb413cd70c1a16bb81572332
https://doi.org/10.1016/j.ast.2015.12.026
https://doi.org/10.1016/j.ast.2015.12.026
Publikováno v:
The Proceedings of the Fluids engineering conference. 2020:OS11-01
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::81685be9aba706605d7d3214fa9319bb
https://doi.org/10.1299/jsmefed.2020.os11-01
https://doi.org/10.1299/jsmefed.2020.os11-01