The effect of hypergravity on the shape of myoblasts by Haruka HINO, Takuya TAMURA, Hiromi SUGIMOTO, Yusuke TAKAHASHI, Shigehiro HASHIMOTO

“…It is already known that micro gravity affects astronaut’s body. In contrary, hyper-gravity might affect myoblasts. …”
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Study of condensation on hydrophobic surface with nanoscale hydrophilic regions by Yutaka YAMADA, Akira KUSABA, Tatsuya IKUTA, Takashi NISHIYAMA, Koji TAKAHASHI, Yasuyuki TAKATA

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Orbital estimation of spacecraft under unknown low-thrust acceleration (First report: estimation of mean orbital elements) by Naoki DATE, Mai BANDO, Shinji HOKAMOTO

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Orbital estimation of spacecraft under unknown low-thrust acceleration (Second report: estimation of osculating orbital elements) by Naoki DATE, Mai BANDO, Shinji HOKAMOTO

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Simultaneous structure design optimization of multiple car models using multiobjective evolutionary algorithm and FEM structure analysis by Akira OYAMA, Takehisa KOHIRA, Tomoaki TATSUKAWA, Takeshi WATANABE, Hiromasa KEMMOTSU

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Study on peristaltic continuous mixing conveyor for composite propellant slurry mixing by Yasuyuki YAMADA, Shun YOSHIHAMA, Akihiro IWASAKI, Kyota ASHIGAKI, Kotaro MATUMOTO, Hiroto HABU, Taro NAKAMURA

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Study on SMA driven hopper design for planetary exploration by Takuma SAKAMOTO, Masatsugu OTSUKI, Takashi KUBOTA

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Three-dimensional internal failure propagation by spherical elastic waves in fused silica glass plate subjected to hypervelocity impact of debris by Mikio NAGANO, Nobuaki KAWAI, Sunao HASEGAWA, Koichi KITAZONO, Eiichi SATO

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Environment recognition through laser-range-finder for small exploration rover by Kai YUN, Shinji HOKAMOTO

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System design of aircraft air conditioning system (3nd Report: Study on the icing analysis for the high-pressure water separation) by Osamu SATO, Hiroshi IWAI, Hideo YOSHIDA

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System design of aircraft air conditioning system (1st report: Effect of component for high-pressure water separation on system operation) by Osamu SATO, Hiroshi IWAI, Hideo YOSHIDA

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System design of aircraft air conditioning system (2nd Report: Study on the simulation modelling of the cross flow heat exchanger) by Osamu SATO, Hiroshi IWAI, Hideo YOSHIDA

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Overturning protection control of lunar-planetary lander with semi-active shock absorber by Takao MAEDA, Masatsugu OTSUKI, Tatsuaki HASHIMOTO

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Conceptual design of single-stage launch vehicle with hybrid rocket engine using design informatics by Kazuhisa CHIBA, Shin'ya WATANABE, Masahiro KANAZAKI, Koki KITAGAWA, Toru SHIMADA

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Special issue on new developments in the field of design and systems engineering 2020 by Akira OYAMA

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Development of mechanical space thermometer for the Tanpopo mission by Hirofumi HASHIMOTO, Eiichi IMAI, Hajime YANO, Hideyuki WATANABE, Shin-ichi YOKOBORI, Akihiko YAMAGISHI

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Crew safety evaluation and injury mechanism at Launch Abort System based on multibody simulation by Shunsuke IMAIZUMI, Akihiro UEDA, Keiichiro FUJIMOTO, Asuka HATANO, Satoshi IZUMI, Shinsuke SAKAI

“…Human space flight vehicle requests a high safety level to protect life of astronauts. Launch Abort System (LAS) is a safety system used to quickly separate the space capsule from its launch vehicle rocket in case of catastrophic failure such as explosion of the vehicle. …”
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Individual drive and control of piezoelectric actuators with a single power supply unit by using variable resistors by Anzu SUMITA, Hiroaki TANAKA, Tadashige IKEDA

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Estimating energy consumption based on natural terrain classification for mobile robots by Kyohei OTSU, Takashi KUBOTA

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Geometrically nonlinear electro-aeroelastic framework for morphing wing with piezoelectric actuators by Natsuki TSUSHIMA, Hitoshi ARIZONO, Tomohiro YOKOZEKI, Kanjuro MAKIHARA

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