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titleM-Vロケット第3段TVCアクチュエータ駆動用高率放電リチウムイオンバッテリ
Other TitleDevelopment of Li-ion battery for the 3rd stage TVC system of the M-V launch vehicle
Author(jpn)森田 泰弘; 曽根 理嗣; 安田 誠一; 佐藤 豊; 長谷川 和雄; 加藤 弘一郎; 中野 隆行
Author(eng)Morita, Yasuhiro; Sone, Yoshitsugu; Yasuda, Seiichi; Sato, Yutaka; Hasegawa, Kazuo; Kato, Koichiro; Nakano, Takayuki
Author Affiliation(jpn)宇宙航空研究開発機構; 宇宙航空研究開発機構; 宇宙航空研究開発機構; アイ・エイチ・アイ・エアロスペース; アイ・エイチ・アイ・エアロスペース; アイ・エイチ・アイ・エアロスペース; アイ・エイチ・アイ・エアロスペース
Author Affiliation(eng)Japan Aerospace Exploration Agency; Japan Aerospace Exploration Agency; Japan Aerospace Exploration Agency; IHI Aerospace Co. Ltd.; IHI Aerospace Co. Ltd.; IHI Aerospace Co. Ltd.; IHI Aerospace Co. Ltd.
Issue Date2005-06
PublisherInstitute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)
宇宙航空研究開発機構宇宙科学研究本部
Publication title第24回宇宙エネルギーシンポジウム 平成16年度
The Twenty-fourth Space Energy Symposium March 7, 2005
Start page17
End page21
Publication date2005-06
Languagejpn
AbstractThe TVC (Thrust Vector Control) system for the 3rd stage of the M-V launch vehicle performs thrust direction control by driving a movable nozzle with two electric actuators, and uses a Silver-Zinc battery to supply 28 V electric power to them. A high-power density battery for launch vehicle did not exist except the Silver-Zinc battery when the M-V TVC system was developed. Therefore, Silver-Zinc battery was adopted, although it has drawbacks of its short storage life and charge/discharge cycle life. After four launches of M-V, this battery system needs to be reconsidered, because of above demerits. The new battery requirements are as follows, (1) Long storage and cycle life, (2) Low cost, (3) Small size and light weight. We selected the lithium ion battery for HEV (Hybrid Electric Vehicle), that can satisfy our requirements. This battery has the following key advantages, (a) High discharge rate, (b) Long life, (c) Low cost, (d) Stabilized Quality, and (e) High safety design. To apply the lithium ion battery for HEV to M-V launch vehicle the following items have been verified. (1) Electrical compatibility with the TVC system of the M-V launch vehicle, (2) Environmental resistance, (3) Space level quality assurance.
Keywordslithium-ion battery; thrust vector control; movable nozzle; actuator; current density; energy density; silver zinc battery; environmental test; shock test; vibration test; リチウムイオン電池; 推力方向制御; 可動ノズル; アクチュエータ; 電流密度; エネルギー密度; 銀亜鉛電池; 環境試験; 衝撃試験; 振動試験
Document TypeConference Paper
JAXA Categoryシンポジウム・研究会
SHI-NOAA0049120004
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/27827


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