日本地球惑星科学連合2019年大会

講演情報

[E] ポスター発表

セッション記号 P (宇宙惑星科学) » P-CG 宇宙惑星科学複合領域・一般

[P-CG21] 宇宙・惑星探査の将来計画と関連する機器開発の展望

2019年5月26日(日) 17:15 〜 18:30 ポスター会場 (幕張メッセ国際展示場 8ホール)

コンビーナ:尾崎 光紀(金沢大学理工研究域電子情報学系)、笠原 慧(東京大学)、亀田 真吾(立教大学理学部)、吉岡 和夫(東京大学大学院新領域創成科学研究科)

[PCG21-P08] A method to quantitatively evaluate Non-evaporable-getter pump for use in space science mission

*西村 晟八1吉川 一朗1吉岡 和夫1荒尾 昇吾1張 天旭1 (1.東京大学)

キーワード:非蒸発型ゲッターポンプ、真空ポンプ

Observation instruments are known to deteriorate under atmospheric condition. Deterioration are mainly caused by reaction with water vapor and oxygen. To prevent this, observation instruments must be maintained under vacuum. The problem is that the conventional vacuum pump are too heavy to carry to the launching site. The need of continuous power supply makes the transport more difficult. Also the vacuum pump must be removed before the launch. These problems are not only making it difficult to maintain observation instruments under vacuum but also causing extra costs. Non-evaporable-getter (NEG) pumps are able to solve these problems. NEG pumps are light weight, compact, oil free, vibration free, and able to operate without energy supply after activation. Considering the utilization of NEG pump for space science missions, we need to quantitatively evaluate the NEG pump to optimize its size, shape, material, and mounting position for each mission. In this study, a method to measure pumping speed of NEG pump for carbon monoxide (as substitute to water vapor and oxygen) was established by using the orifice method. By using this method, it will be able to develop a NEG pump which best applies the case for each mission.