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18 results on '"Sugimori, Daizo"'

3. Capacitive Void Fraction Sensor for Ground Test of LE-5B-3

Author

Sakamoto, Yuki, Kobayashi, Hiroaki, Higashi, Kazuhiro, Nagao, Naoki, Sugimori, Daizo, Kinefuchi, Kiyoshi, and Sato, Tetsuya

Subjects
Capacitive Sensor, LE-5B-3 Engine, Cryogenic, Void Fraction, Liquid Hydrogen
Abstract

Accepted: 2018-07-17, 資料番号: SA1180335000

Published
2019

5. Sounding Rocket Experiment on Chill-down Process with Liquid Nitrogen

Author

Himeno, Takehiro, Haba, Daichi, Sarae, Wataru, Kinefuchi, Kiyoshi, Umemura, Yutaka, Yabusaki, Daisuke, Sugimori, Daizo, Kobayashi, Hiroaki, Nonaka, Satoshi, and Sato, Tetsuya

Subjects
Sounding Rocket, Cryogenic, Two-phase Flow, Microgravity, Propellant Management
Abstract

平成29年度衝撃波シンポジウム (2018年3月7日-9日. 東北大学片平さくらホール ）仙台市, 宮城県, (2018年3月7日-9日. 宇宙航空研究開発機構角田宇宙センター ）角田市, 宮城県, Symposium on Shock Waves in Japan, FY2017 (March 7-9, 2018. Sakura Hall), Sendai, Miyagi, (March 7-9, 2018. Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC)), Kakuda, Miyagi, 資料番号: SA6000119061, レポート番号: 2A2-2

Published
2018

6. H3ロケット開発状況と技術課題取組事例の紹介

Author

Sugimori, Daizo

Abstract

平成29年度宇宙輸送シンポジウム（2018年1月18日-19日. 宇宙航空研究開発機構宇宙科学研究所（JAXA)(ISAS)）, 相模原市, 神奈川県, Space Transportation Symposium FY2017 (January 18-19, 2018. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, 資料番号: SA6000210040, レポート番号: STCP-2017-040

Published
2018

7. H3開発で取組む推進薬マネジメント技術

Author

Sugimori, Daizo

Abstract

平成27年度宇宙輸送シンポジウム（2016年1月14日-15日. 宇宙航空研究開発機構宇宙科学研究所（JAXA)(ISAS)）, 相模原市, 神奈川県, Space Transportation Symposium FY2015 (January 14-15, 2016. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, 資料番号: SA6000050013, レポート番号: STCP-2015-014

Published
2016

9. 基幹ロケット上段推進系の発展と国際有人探査への貢献 －極低温軌道間輸送機の研究開発－

Author

Kinefuchi, Kiyoshi, Saitoh, Yasuhiro, Nishihira, Shintaro, Sarae, Wataru, Sugimori, Daizo, Okita, Koichi, Tani, Naoki, Umemura, Yutaka, Kobayashi, Hiroaki, Himeno, Takehiro, Ishikawa, Keitaro, and Aoyama, Taichi

Subjects
Launch Vehicle, Upper Stage, Cryogenic Propulsion, Propellant Management
Abstract

第57回宇宙科学技術連合講演会（2013年10月9日-11日. 米子コンベンションセンター（BiG SHiP）), 米子市, 鳥取県, Upper stages of H-IIA and H-IIB use LOX/LH2 as a propellant and achieve high performance and reliability. Utilizingthe experiences of cryogenic propellant management, the upper stage of H-IIA is now being upgraded for more efficientmass transfer. The propulsion system development is one of the most critical issues for the H-IIA Upgrade, and willsucceed CPS, Cryogenic Propulsion Stage, which is an element of the international exploration architecture for thein-space orbital transfer. Currently, CPS was scaled up to DUUS, Dual Use Upper Stage, and JAXA is now conducting acollaborative study with NASA. It is necessary to improve understanding of cryogenic propellant management to developDUUS, hence, JAXA focuses on not only vehicle development but also basic researches with universities and industries., 資料番号: AC1400031000, レポート番号: JSASS-2013-4163

Published
2013

10. 液体ロケットの推進薬タンクにおけるスロッシングと圧力変動予測へ向けた取組み

Author

Himeno, Takehiro, Nonaka, Satoshi, Naruo, Yoshihiro, Umemura, Yutaka, Ishikawa, Katsutoshi, Uzawa, Seiji, Watanabe, Toshinori, Sugimori, Daizo, Kinebuchi, Kiyoshi, and Okita, Koichi

Abstract

平成23年度宇宙輸送シンポジウム（2012年1月19日-20日. 宇宙航空研究開発機構宇宙科学研究所（JAXA)（ISAS)）, 相模原市, 神奈川県, Space Transportation Symposium FY2011 (January 19-20, 2012. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, 著者人数: 11名, 資料番号: SA6000003016, レポート番号: STCP-2011-016

Published
2012

11. Sounding Rocket Experiment on Chill-down Process with Liquid Nitrogen in a Complex Channel

Author

Sarae, Wataru, primary, Kinefuchi, Kiyoshi, additional, Yabusaki, Daisuke, additional, Sugimori, Daizo, additional, Fujita, Takeshi, additional, Okita, Koichi, additional, Umemura, Yutaka, additional, Fujimoto, Keiichiro, additional, Negishi, Hideyo, additional, Kobayashi, Hiroaki, additional, Himeno, Takehiro, additional, Sato, Tetsuya, additional, and Nonaka, Satoshi, additional

Published
2015
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12. Measuring Two-phase Flow Behavior and Heat Transfer Characteristics during Coasting Flight, Development of Experimental Equipment for S-310-43 Sounding Rocket

Author

KOBAYASHI, Hiroaki, primary, KINEFUCHI, Kiyoshi, additional, SARAE, Wataru, additional, UMEMURA, Yutaka, additional, FUJIMOTO, Keiichiro, additional, YABUSAKI, Daisuke, additional, SUGIMORI, Daizo, additional, HIMENO, Takehiro, additional, SATO, Tetsuya, additional, KITAKOGA, Satoshi, additional, SUMI, Yuki, additional, SAKAMOTO, Yuki, additional, NONAKA, Satoshi, additional, and FUJITA, Takeshi, additional

Published
2015
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15. Investigation on Pressure Change Induced by Cryogenic Sloshing

Author

Himeno, Takehiro, primary, Ishikawa, Katsutoshi, additional, Umemura, Yutaka, additional, Inoue, Chihiro, additional, Watanabe, Toshinori, additional, Nonaka, Satoshi, additional, Naruo, Yoshihiro, additional, Inatani, Yoshifumi, additional, Kinefuchi, Kiyoshi, additional, Sugimori, Daizo, additional, and Okita, Koichi, additional

Published
2012
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16. Heat Exchange and Pressure Drop Enhanced by Sloshing

Author

Himeno, Takehiro, primary, Sugimori, Daizo, additional, Ishikawa, Katsutoshi, additional, Umemura, Yutaka, additional, Uzawa, Seiji, additional, Inoue, Chihiro, additional, Watanabe, Toshinori, additional, Nonaka, Satoshi, additional, Naruo, Yoshihiro, additional, Inatani, Yoshifumi, additional, Kinefuchi, Kiyoshi, additional, Yamashiro, Ryoma, additional, Morito, Toshiki, additional, and Okita, Koichi, additional

Published
2011
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