TY - GEN
T1 - Expantion and measurement of spiral foldedmembrane by small satellite
AU - Miyashita, Tomoyuki
AU - Yamakawa, Hiroshi
AU - Katsumata, Nobuhisa
AU - Natori, Michihiro C.
N1 - Funding Information:
The authors thank the member of Ultra Light Weight Space Structure (ULWSS) research group in Waseda University. Mr. Kaneshiro, Mr. Komoda, Mr. Kameyama, Mr. Sakamoto and Mr. Nishijima were very active members and we express special thanks. This work was partially supported by JSPS KAKENHI Grant Number 16K14507.
Publisher Copyright:
© 2017 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
Copyright:
Copyright 2017 Elsevier B.V., All rights reserved.
PY - 2017
Y1 - 2017
N2 - The small sattelites become popular due to the development of electrical parts and frequent launch opportunities. In this sudy, we will introduce one of our missions on orbit by 1U size small satellite Waseda-SAT3. This satellite have two main missions. One is thermal active control by soft matter and the other is measurement of shpe of membrane expanded from spiral folded shape supported by hinge-less mast. The membrane installed in this satellite has parabolic surface and painted innerside to measure shape by lattice projection method and equips solor cell outside to show effectiveness of spiral folding theory considering thickness effect of the membrane.
AB - The small sattelites become popular due to the development of electrical parts and frequent launch opportunities. In this sudy, we will introduce one of our missions on orbit by 1U size small satellite Waseda-SAT3. This satellite have two main missions. One is thermal active control by soft matter and the other is measurement of shpe of membrane expanded from spiral folded shape supported by hinge-less mast. The membrane installed in this satellite has parabolic surface and painted innerside to measure shape by lattice projection method and equips solor cell outside to show effectiveness of spiral folding theory considering thickness effect of the membrane.
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U2 - 10.2514/6.2017-0848
DO - 10.2514/6.2017-0848
M3 - Conference contribution
AN - SCOPUS:85017266655
T3 - AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting
BT - AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 55th AIAA Aerospace Sciences Meeting
Y2 - 9 January 2017 through 13 January 2017
ER -