首页> 外军国防科技报告 >Design of a hermetically sealing inlet for in-situ planetary exploration;
【2h】

Design of a hermetically sealing inlet for in-situ planetary exploration;

机译:设计用于原位行星探测的密封入口;

代理获取
代理获取并翻译 | 示例

摘要

A miniature low-powered life detection device for in-situ isolation and sequencing of nucleic acids is to be used to test the hypothesis of a plausible shared ancestry due to meteoric exchange between Earth and Mars. The soil sample collection inlet is a critical part of the device. The following paper presents a design review of previous inlet mechanisms and an inlet design proposal for in-situ planetary exploration. The key attributes of the design are the sealing interfaces and an inverted dovetail cross sectional geometry for a linear carriage. The inlet emphasizes a design for manufacturability, weight savings, durability, and many cycles. Based on the established fundamental requirements, the design is evaluated on the thermal analysis at the extreme theoretical temperatures and the force, power, and energy required to actuate and seal the inlet, using Finite Element Analysis and numerical computation. The design successfully meets the majority of the fundamental requirements. The modularity and low required actuation force of the design are applicable to many current and future space instruments.;

著录项

  • 作者

  • 作者单位
  • 年(卷),期 2019(),
  • 年度 2019
  • 页码
  • 总页数 106
  • 原文格式 PDF
  • 正文语种
  • 中图分类
  • 网站名称 数字空间系统
  • 栏目名称 所有文件
  • 关键词

  • 入库时间 2022-08-19 17:00:20
代理获取

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号