Zobrazeno 1 - 10
of 16
pro vyhledávání: '"Ideo Masuda"'
Autor:
Katsumi Miyama, Taiichi Nagata, Shigeru Saito, Toshiyuki Takashima, Ideo Masuda, Toshio Narita, Kenichi Kajiwara
Publikováno v:
MATERIALS TRANSACTIONS. 55:298-303
The compositions with tie-lines between the », ·, £, i, and Nb(Cr,Re)2 phases in a ternary ReCrNb system were investigated at 1500°C by heat-treating various ternary ReCrNb alloys in vacuum for either 2 or 220h. The microstructures of the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ff69366f849bd1337f480e9ad965ba6e
https://doi.org/10.2320/matertrans.m2013282
https://doi.org/10.2320/matertrans.m2013282
Autor:
Sakaguchi Hiroyuki, Hideaki Nanri, Ishikawa Yasuhiro, Ideo Masuda, Hiroya Asakawa, Ryuu Shinohara
Publikováno v:
52nd AIAA/SAE/ASEE Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2a06b16b0a041f9d9318efabbfa543ac
https://doi.org/10.2514/6.2016-5078
https://doi.org/10.2514/6.2016-5078
Publikováno v:
Space Safety is No Accident ISBN: 9783319159812
Payloads launched from JAXA Launch Facilities must meet JAXA safety requirements. For one, payloads having liquid propulsion systems are required to have triple seals to prevent propellant leakage.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b6cf42cde5f706031fc35787e11688c3
https://doi.org/10.1007/978-3-319-15982-9_23
https://doi.org/10.1007/978-3-319-15982-9_23
Autor:
Tadashi Masuoka, Hirohide Ikeda, Hideshi Kagawa, Daijiro Ishida, Kazuki Mouri, Keisuke Yamada, Mamoru Takahashi, Ideo Masuda
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Satellite components falling to the ground are a crucial problem, particularly titanium tanks in propulsion systems. Satellite tanks are generally made of titanium alloy because it is light and compatible with propellants used for the satellite. Howe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8b42c81f929875145940aabb83a2e185
https://doi.org/10.2514/6.2014-3995
https://doi.org/10.2514/6.2014-3995
Publikováno v:
Journal of Spacecraft and Rockets. 38:417-425
Hydrogen atoms were probed in the near-e eld plume of a 1.8-kW e ight-type arcjet thruster, using two-photon laser-induced e uorescence. The arcjet was operated on an N 2/H2 gas mix simulating hydrazine decomposition products. Thevelocity distributio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dbff61b656f8049f72ef0e2ad02afdde
https://doi.org/10.2514/2.3700
https://doi.org/10.2514/2.3700
Publikováno v:
Journal of Spacecraft and Rockets. 38:79-86
Density, velocity, and temperature data were obtained in the near-e eld plume of a 1.8-kW hydrazine arcjet thruster, using the NH molecule as a probe. This was the e rst laser spectroscopic study on a e ight-type arcjet. The rotational temperature of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0d3f9e9fa5a83ea7b9d63a8e2f9c7b98
https://doi.org/10.2514/2.3657
https://doi.org/10.2514/2.3657
Publikováno v:
49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::29a08c2f2208426cbd71fcd7fe838ea5
https://doi.org/10.2514/6.2013-3984
https://doi.org/10.2514/6.2013-3984
Publikováno v:
49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Because the titanium tank is one of the greatest ground-damaging component when a low-Earth orbit satellite falls to ground, we plan to replace the general titanium propellant tank with a reentry melting promotion-type tank to reduce the ground hazar
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4f8d7b5dc6a64839a82a85fa9c1d3180
https://doi.org/10.2514/6.2013-3985
https://doi.org/10.2514/6.2013-3985
Autor:
Shinichi MORIYA, Takuma INOUE, Masahiro SASAKI, Takayuki NAKAMOTO, Takahiro KIMURA, Naoyuki NOMURA, Keiko KIKUCHI, Akira KAWASAKI, Toshiki KATO, Ideo MASUDA
Publikováno v:
Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan; 2018, Vol. 16 Issue 3, p261-266, 6p
Autor:
Ideo Masuda, Kenichi Kajiwara
Publikováno v:
47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
We choose a plug cluster nozzle targeting use with geostationary satellites, from the perspective of installation restrictions on rockets and performance improvement. The flow properties were determined via tests and analysis using a feasibility samp
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dbed0a2b51c7ad80838b5463d8d11e9a
https://doi.org/10.2514/6.2011-5941
https://doi.org/10.2514/6.2011-5941