抄録
Space inflatable actuated rod (SPINAR) has been developed as an ultra-light one-dimensional extendible structure driven by an inflatable actuator. SPINAR satisfies ever-intensifying requirements such as lightweight, high rigidity, high strength, high packaging efficiency, favorable antenna performance and simple extension mechanisms. Performed were the analysis of the requirements for structural design of one-dimensional extendible antenna structure and the detailed conceptual design for a scientific mission under consideration in ISAS/JAXA, and the advantages of the inflatable-assisted structure were evaluated. The rod of SPINAR consists of tri-axially woven fiber composite materials and thin inflatable tube. The extension tests were successful at any direction with respect to the gravity. Spin extension tests on a turntable also showed smooth extension. Spin extension test of SPINAR on a turntable under micro-gravity environment using airplane parabolic flight was performed in August 2005, and the test showed that SPINAR would satisfy the requirements for the science mission. The composite rod was tested as an antenna in radio wave environment, and the material was selected to use as a dipole antenna for a high-resolution electric-field sensor. SPINAR is expected not only to use as an antenna rod, but also to explore a broad range of application opportunities as an excellent substitute for conventional mechanical deployable structures.
元の言語 | English |
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ホスト出版物のタイトル | Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference |
ページ | 2613-2619 |
ページ数 | 7 |
巻 | 4 |
出版物ステータス | Published - 2006 |
イベント | 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference - Newport, RI 継続期間: 2006 5 1 → 2006 5 4 |
Other
Other | 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference |
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市 | Newport, RI |
期間 | 06/5/1 → 06/5/4 |
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ASJC Scopus subject areas
- Architecture
これを引用
Design and evaluation of an ultra-light extendible mast as an inflatable structure. / Higuchi, Ken; Watanabe, Kazuki; Watanabe, Akihito; Tsunoda, Hiroaki; Yamakawa, Hiroshi.
Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 巻 4 2006. p. 2613-2619.研究成果: Conference contribution
}
TY - GEN
T1 - Design and evaluation of an ultra-light extendible mast as an inflatable structure
AU - Higuchi, Ken
AU - Watanabe, Kazuki
AU - Watanabe, Akihito
AU - Tsunoda, Hiroaki
AU - Yamakawa, Hiroshi
PY - 2006
Y1 - 2006
N2 - Space inflatable actuated rod (SPINAR) has been developed as an ultra-light one-dimensional extendible structure driven by an inflatable actuator. SPINAR satisfies ever-intensifying requirements such as lightweight, high rigidity, high strength, high packaging efficiency, favorable antenna performance and simple extension mechanisms. Performed were the analysis of the requirements for structural design of one-dimensional extendible antenna structure and the detailed conceptual design for a scientific mission under consideration in ISAS/JAXA, and the advantages of the inflatable-assisted structure were evaluated. The rod of SPINAR consists of tri-axially woven fiber composite materials and thin inflatable tube. The extension tests were successful at any direction with respect to the gravity. Spin extension tests on a turntable also showed smooth extension. Spin extension test of SPINAR on a turntable under micro-gravity environment using airplane parabolic flight was performed in August 2005, and the test showed that SPINAR would satisfy the requirements for the science mission. The composite rod was tested as an antenna in radio wave environment, and the material was selected to use as a dipole antenna for a high-resolution electric-field sensor. SPINAR is expected not only to use as an antenna rod, but also to explore a broad range of application opportunities as an excellent substitute for conventional mechanical deployable structures.
AB - Space inflatable actuated rod (SPINAR) has been developed as an ultra-light one-dimensional extendible structure driven by an inflatable actuator. SPINAR satisfies ever-intensifying requirements such as lightweight, high rigidity, high strength, high packaging efficiency, favorable antenna performance and simple extension mechanisms. Performed were the analysis of the requirements for structural design of one-dimensional extendible antenna structure and the detailed conceptual design for a scientific mission under consideration in ISAS/JAXA, and the advantages of the inflatable-assisted structure were evaluated. The rod of SPINAR consists of tri-axially woven fiber composite materials and thin inflatable tube. The extension tests were successful at any direction with respect to the gravity. Spin extension tests on a turntable also showed smooth extension. Spin extension test of SPINAR on a turntable under micro-gravity environment using airplane parabolic flight was performed in August 2005, and the test showed that SPINAR would satisfy the requirements for the science mission. The composite rod was tested as an antenna in radio wave environment, and the material was selected to use as a dipole antenna for a high-resolution electric-field sensor. SPINAR is expected not only to use as an antenna rod, but also to explore a broad range of application opportunities as an excellent substitute for conventional mechanical deployable structures.
UR - http://www.scopus.com/inward/record.url?scp=34147168224&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=34147168224&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:34147168224
SN - 1563478080
SN - 9781563478086
VL - 4
SP - 2613
EP - 2619
BT - Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
ER -