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Uncertainty quantification on satellite thermal design

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EG3288 Subject Category: Research and Development PDF Responsible Representative: Eiji Shima, Research and Development Directorate, Research Unit Contact Information: Hiroshi Kato kato.hiroshi@jaxa.jp Members: Hiroshi Kato Abstract Our purpose is to improving the satellite thermal design process by developing a key technology of "satellite thermal environment uncertainty quantification". Reference URL N/A Reasons for using JSS2 There is no environment to perform the satellite thermal analyses of numerous samples under realistic time.・・・<<read more>>

Fundamental Studies of Methane RCS

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EG3500 Subject Category: Research and Development PDF Responsible Representative: Daiki Terakado, Research and Development Directorate, Research Unit IV Contact Information: Daiki Terakado terakado.daiki@jaxa.jp Members: Daiki Terakado Abstract The present RCS of hydrazine used for controling rockets has a weak point on its toxicity. The present project focuses on the non-toxic property of methane and develops safer RCS system for the future rockets. Reference URL N/A Reasons for using JSS2 The・・・<<read more>>

Construction and maintenance of quality engineering tools

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EH2900 Subject Category: Common Business PDF Responsible Representative: Yuji KADO, Safety and Mission Assurance Department Contact Information: Yuji KADO kado.yuji@jaxa.jp Members: Yuji Kado, Hiroshi Yanaka Abstract Application of optimization software to JSS Reference URL N/A Reasons for using JSS2 To reduce the calculation time of the simulation Achievements of the Year We found that our In-house optimization software could be used by JSS. Publications N/A Usage of JSS2 Computational Information・・・<<read more>>

Numerical Analysis of aerodynamic characteristics on H3 launch vehicle

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EK2300 Subject Category: Space Technology PDF Responsible Representative: Masashi Okada, Space Technology Directorate 1, H3 Projcet Team Contact Information: Hiroshi Ikaida ikaida.hiroshi@jaxa.jp Members: Hiroshi Ikaida, Kazuhiro Imai, Fumihiro Itoo Abstract From the viewpoint of international competitiveness, develop a new launch system with low cost and high performance. Reference URL N/A Reasons for using JSS2 Aerodynamic data and load analysis resuls are necessary to confirm the feasibility in the H3 launch・・・<<read more>>

Numerical Simulations for H3 Rocket Development

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EK2302 Subject Category: Space Technology PDF Responsible Representative: Masashi Okada, Space Technology Directorate, H3 Project Team Contact Information: Hideyo Negishi negishi.hideyo@jaxa.jp Members: Seiji Tsutsumi, Masashi Kanamori, Hiroaki Amakawa, Masaaki Ino, Hironori Fujiwara, Masaharu Abe, Hiroyuki Ito, Shinji Ohno, Takenori Nakajima, Hideyo Negishi, Yu Daimon, Takanori Haga, Taro Shimizu, Junya Aono, Tetsufumi Ohmaru Abstract Please refer to the following URL: http://global.jaxa.jp/projects/rockets/h3/ Reference URL Please refer to 'JAXA | H3 Launch Vehicle'.・・・<<read more>>