Výsledky vyhledávání - "Tsutomu Fukatsu"

Keeper Ignition and Discharge Characteristics of Hollow Cathode Center-Mounted on Hall Thruster

Autor: Ryudo Tsukizaki, Ikkoh Funaki, Tsutomu Fukatsu, Kiyoshi Kinefuchi, Yosuke Tashiro, Taizo Shiiki, Shinatora Cho, Yuya Hirano

Publikováno v: Journal of Propulsion and Power. 37(2):1-8

形態: カラー図版あり
Physical characteristics: Original contains color illustrations
Accepted: 2020-08-25
資料番号: PA2010026000

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1e177aef9011d82ba9dd103ed23ea71e
http://id.nii.ac.jp/1696/00047485/

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The Compatibility Evaluation Method of the 500N ^|^amp; 120N Japanese Bi-Propellant Thrusters with the HTV System ^|^amp; Operation Design

Autor: Hiroshi Sasaki, Tsutomu Fukatsu, Katsuhiko Sugimori, Shinichi Takata

Publikováno v: TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN. 12:Pg_7-Pg_15

This paper describes the evaluation method of the new Japanese thrusters design, balancing and verification of interface compatibility with the HTV system and operation design. Thruster performance directly affects the performance of the space craft.

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::dd2c4332964e3a95b4979465c0c7581b
https://doi.org/10.2322/tastj.12.pg_7

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Akademický článek

1,000-hours Demonstration of a 6-kW-class Hall Thruster for All-Electric Propulsion Satellite.

Autor: Ikkoh FUNAKI, Shinatora CHO, Tadahiko SANO, Tsutomu FUKATSU, Yosuke TASHIRO, Taizo SHIIKI, Yoichiro NAKAMURA, Hiroki WATANABE, Kenichi KUBOTA, Yoshiki MATSUNAGA, Kenji FUCHIGAMI

Publikováno v: Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan; 2019, Vol. 17 Issue 5, p589-595, 7p

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HTV Thermal Control Architecture and First Flight Results

Autor: Ikuo Ohsawa, Keita Fukuzawa, Takafumi Matsuda, Tsutomu Fukatsu, Tatsuya Sato, Takeshi Kamiya, Hajime Mitsuki

Publikováno v: 40th International Conference on Environmental Systems.

The H-II Transfer Vehicle (HTV), designed and built in Japan, is one of unmanned cargo transfer spacecrafts and the HTV-1 was launched in September, 2009 as a first flight. The HTV-1 was docked to the ISS a week after the launch and had been attached

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::3d10d900beaebb275666a8005abb9973
https://doi.org/10.2514/6.2010-6221

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