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Advances in Space Research | 2018

A Balloon-Borne Very Long Baseline Interferometry Experiment in the Stratosphere: Systems Design and Developments

Akihiro Doi; Yusuke Kono; Kimihiro Kimura; Satomi Nakahara; Tomoaki Oyama; Nozomi Okada; Yasutaka Satou; Kazuyoshi Yamashita; Naoko Matsumoto; Mitsuhisa Baba; Daisuke Yasuda; Shunsaku Suzuki; Yutaka Hasegawa; Mareki Honma; Hiroaki Tanaka; Kosei Ishimura; Yasuhiro Murata; Reiho Shimomukai; Tomohiro Tachi; Kazuya Saito; Naohiko Watanabe; Nobutaka Bando; Osamu Kameya; Yoshinori Yonekura; Mamoru Sekido; Yoshiyuki Inoue; Hikaru Sakamoto; Nozomu Kogiso; Yasuhiro Shoji; Hideo Ogawa

Abstract The balloon-borne very long baseline interferometry (VLBI) experiment is a technical feasibility study for performing radio interferometry in the stratosphere. The flight model has been developed. A balloon-borne VLBI station will be launched to establish interferometric fringes with ground-based VLBI stations distributed over the Japanese islands at an observing frequency of approximately 20u202fGHz as the first step. This paper describes the system design and development of a series of observing instruments and bus systems. In addition to the advantages of avoiding the atmospheric effects of absorption and fluctuation in high frequency radio observation, the mobility of a station can improve the sampling coverage (“uv-coverage”) by increasing the number of baselines by the number of ground-based counterparts for each observation day. This benefit cannot be obtained with conventional arrays that solely comprise ground-based stations. The balloon-borne VLBI can contribute to a future progress of research fields such as black holes by direct imaging.


2018 AIAA Spacecraft Structures Conference | 2018

Effects of Elasto-Plastic Behavior of Crease on Deployed Shape of Space Membrane

Yasutaka Satou; Hiroshi Furuya


The Proceedings of Mechanical Engineering Congress, Japan | 2015

S1910202 Development of Boom-Membrane Deployable Space Structures for De-orbiting Satellites

Hiroshi Furuya; Yasutaka Satou; Moto Takai; Hiraku Sakamoto; Nobukatsu Okuizumi


Archive | 2014

Deployment Experiment of Boom-Membrane Integrated Wrapped Structures

Hiroshi Furuya; Yasutaka Satou; Hiraku Sakamoto; M. C. Natori; Nobukatsu Okuizumi; 寛 古谷; 泰貴 佐藤; 啓 坂本; 通弘 名取; 信克 奥泉


Archive | 2014

次期ソーラー電力セイルに向けた大型膜面の収納・展開・展張法の検討

洋次 白澤; 信克 奥泉; 三郎 松永; 寛 古谷; 啓 坂本; 泰貴 佐藤; 弘 山浦; 通弘 名取; 康行 宮崎; 純 松本; 剛 大野; 俊大 中条; 直宏 林; 拓 濱崎; 隼仁 菊池; 祐貴 寺元; 省吾 門西; 歩 山崎; 匡士 西澤; 剛志 佐藤; 孝 長洲; 千恵 根本; 遼太 井上; 主 水森; Yoji Shirasawa; Nobukatsu Okuizumi; Saburo Matunaga; Osamu Mori; Hiroshi Furuya; Hiraku Sakamoto


The Proceedings of Mechanical Engineering Congress, Japan | 2013

J191015 Design and Demonstration of Rib-Stiffened Shell Antenna Based on Simultaneous Optimization of Structure and Actuator Locations

Yasutaka Satou; Hiroshi Furuya; Nozomu Kogiso


The Proceedings of Mechanical Engineering Congress, Japan | 2012

J191024 One-Dimensional Deployment Properties of Creased Membrane

Yasutaka Satou; Hiroshi Furuya


The Proceedings of Mechanical Engineering Congress, Japan | 2011

J191062 FEM Analyses of Local Buckling Induced by Wrapping Fold of Large Membrane

Yasutaka Satou; Hiroshi Furuya


The proceedings of the JSME annual meeting | 2010

S1903-1-5 Preliminary Experiment of Wrapping Fold Membrane

Yasutaka Satou; Hiroshi Furuya


The proceedings of the JSME annual meeting | 2009

S1903-1-6 Precise Folding of Two-dimensional Deployable Membrane with Guided-pin

Yasutaka Satou; Hiroshi Furuya

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Hiroshi Furuya

Tokyo Institute of Technology

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Hiraku Sakamoto

Tokyo Institute of Technology

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Nobukatsu Okuizumi

Japan Aerospace Exploration Agency

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Nozomu Kogiso

Osaka Prefecture University

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啓 坂本

Tokyo Institute of Technology

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Akihiro Doi

Japan Aerospace Exploration Agency

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Daisuke Yasuda

Osaka Prefecture University

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Hideo Ogawa

Osaka Prefecture University

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Hikaru Sakamoto

Tokyo Institute of Technology

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Hiroaki Tanaka

National Defense Academy of Japan

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