PTFE as a viable sealing material for lightweight mass spectrometry ovens in dusty extraterrestrial environments

Feargus A J Abernethy, Hannah Chinnery, Robert Lindner, Simeon J Barber
{"title":"PTFE as a viable sealing material for lightweight mass spectrometry ovens in dusty extraterrestrial environments","authors":"Feargus A J Abernethy, Hannah Chinnery, Robert Lindner, Simeon J Barber","doi":"10.1093/rasti/rzae003","DOIUrl":null,"url":null,"abstract":"\n Ever increasing interest in the Moon, not only for scientific but also commercial and prospecting purposes, requires a more streamlined and reproduceable approach to issues such as the sealing of sample handling ovens, in contrast to the mission-specific mechanisms which have tended to prevail in the past. A test breadboard has been designed and built in order to evaluate the leak rates of different oven sealing concepts and materials within the context of the ProSPA instrument being developed for the European Space Agency. Sealing surface geometries based on a simple 90° knife-edge, and two widely used vacuum fitting standards (VCR® and ConFlat®) have been tested using PTFE gaskets in vacuum across a temperature range of -100°C to 320°C, equivalent to a projected -100°C to 1000°C sample heating range in the ProSPA ovens. The impact of using glass- and carbon- filled PTFE has also been investigated, as has the effect of dust coverage of JSC-1A lunar simulant up to 9 per cent by area. The best combination of properties appears to be unfilled PTFE, compressed between two 90° knife-edges with a confining force of ∼ 400 N. This can produce a leak rates within the 10−7 Pa.m3.s−1 range or better regardless of the level of dust applied within the experimental constraints. A strong temperature-dependence on the leak rate is identified, meaning that careful oven design will be required to minimise the temperature at the seal interface even within the operational temperature range PTFE itself.","PeriodicalId":500957,"journal":{"name":"RAS Techniques and Instruments","volume":"119 22","pages":""},"PeriodicalIF":0.0000,"publicationDate":"2024-02-10","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"RAS Techniques and Instruments","FirstCategoryId":"0","ListUrlMain":"https://doi.org/10.1093/rasti/rzae003","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

Abstract

Ever increasing interest in the Moon, not only for scientific but also commercial and prospecting purposes, requires a more streamlined and reproduceable approach to issues such as the sealing of sample handling ovens, in contrast to the mission-specific mechanisms which have tended to prevail in the past. A test breadboard has been designed and built in order to evaluate the leak rates of different oven sealing concepts and materials within the context of the ProSPA instrument being developed for the European Space Agency. Sealing surface geometries based on a simple 90° knife-edge, and two widely used vacuum fitting standards (VCR® and ConFlat®) have been tested using PTFE gaskets in vacuum across a temperature range of -100°C to 320°C, equivalent to a projected -100°C to 1000°C sample heating range in the ProSPA ovens. The impact of using glass- and carbon- filled PTFE has also been investigated, as has the effect of dust coverage of JSC-1A lunar simulant up to 9 per cent by area. The best combination of properties appears to be unfilled PTFE, compressed between two 90° knife-edges with a confining force of ∼ 400 N. This can produce a leak rates within the 10−7 Pa.m3.s−1 range or better regardless of the level of dust applied within the experimental constraints. A strong temperature-dependence on the leak rate is identified, meaning that careful oven design will be required to minimise the temperature at the seal interface even within the operational temperature range PTFE itself.
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
将聚四氟乙烯作为地外多尘环境中轻质质谱烤箱的可行密封材料
人们对月球的兴趣与日俱增,这不仅是出于科学研究的目的,也是出于商业和勘探的目的,这就要求在诸如样品处理炉的密封等问题上采用一种更加简化和可复制的方法,而不是像过去那样采用针对特定任务的机制。为了在为欧洲航天局开发的 ProSPA 仪器范围内评估不同烤箱密封概念和材料的泄漏率,我们设计并建造了一个测试面包板。在-100°C 至 320°C(相当于 ProSPA 烤箱中预计的-100°C 至 1000°C 样品加热范围)的真空条件下,使用聚四氟乙烯垫片对基于简单 90° 刀刃的密封面几何形状和两种广泛使用的真空配件标准(VCR® 和 ConFlat®)进行了测试。此外,还研究了使用玻璃和碳填充聚四氟乙烯的影响,以及 JSC-1A 月球模拟物灰尘覆盖率高达 9% 面积的影响。最好的特性组合似乎是未填充的聚四氟乙烯,在两个 90° 的刀刃之间压缩,限制力为 400 N。泄漏率与温度密切相关,这意味着即使在聚四氟乙烯本身的工作温度范围内,也需要精心设计烘箱,以尽量降低密封界面的温度。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 去求助
来源期刊
自引率
0.00%
发文量
0
期刊最新文献
The exosphere of Mars can be tracked by a high-spectral resolution telescope, such as the Line Emission Mapper Training a convolutional neural network for real-bogus classification in the ATLAS survey Exoplanet host star classification: Multi-Objective Optimisation of incomplete stellar abundance data PTFE as a viable sealing material for lightweight mass spectrometry ovens in dusty extraterrestrial environments PTFE as a viable sealing material for lightweight mass spectrometry ovens in dusty extraterrestrial environments
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1