首页> 外文会议>International Astronautical Congress >STRUCTURE DEVELOPMENT OF THE HP3 INSTRUMENT SUPPORT SYSTEM FOR THE MARS MISSION INSIGHT
【24h】

STRUCTURE DEVELOPMENT OF THE HP3 INSTRUMENT SUPPORT SYSTEM FOR THE MARS MISSION INSIGHT

机译:MARS任务洞察HP3仪器支持系统的结构开发

获取原文

摘要

On May 05, 2018 NASA JPL launched its mission to Mars called "InSight". Main objective of this mission is to gain more knowledge of the evolution of terrestrial planets. Beside a number of different scientific instruments onboard the lander there are two instruments that will perform measurements on the Martian ground. One of the instruments is HP3 (Heat Flow and Physical Properties Package), which was developed by the German Aerospace Center (DLR) to measure the heat flow of the Martian outer crust. It uses a hammering mechanism equipped with heating foils on the outer hull to pull a tether approx. 5 m into the soil. The tether is equipped with temperature elements for the determination of temperature gradients in the ground. There is the need of a separate system to be able to perform those activities on the surface. This system is called the "HP3 Support System". Its main task is to ensure a stable, nearly perpendicular position of the hammering mechanism relative to the soil on the Martian surface before initial penetration. It furthermore houses the instruments for length measurement and serves as electrical connection to the lander. The paper will give an overview of the development and the qualification of the structure of the Support System. It will focus on the mechanical design, the analysis of the structural dynamics but in particular on the testing which includes standard environmental testing but also numerous development tests that are very mission specific. The mechanical design of the Support System is mainly driven by a unique set of requirements derived from the working environment on Mars, the deployment from the lander deck and the mechanically separated operation on the surface. The instrument design will be explained to show which design elements were implemented to ensure proper functionality. Various development tests had to be performed during the Support System structure development. Besides the standard qualification tests, special qualifi
机译:2018年5月5日,美国国家航空航天党杰出·杰普推出了被称为“洞察力”的马斯的使命。这项任务的主要目标是获得更多对陆地行星演变的了解。在船上许多不同的科学仪器旁边,兰德有两种仪器将在火星地面上进行测量。其中一个仪器是HP3(热流和物理性质包),由德国航空航天中心(DLR)开发,以测量火星外壳的热流。它采用了一个锤击机构,在外壳上配备了加热箔,以拉紧约束。 5米进入土壤。系绳配有温度元件,用于确定地面温度梯度。需要单独的系统能够在表面上执行这些活动。该系统称为“HP3支持系统”。其主要任务是确保在初始渗透前相对于火星表面上的土壤稳定,几乎垂直的锤击地位。此外,它还容纳了长度测量的仪器,用作与着陆器的电气连接。本文将概述支持系统结构的开发和资格。它将专注于机械设计,对结构动态的分析,但特别是在测试中,包括标准环境测试,而且还具有特定任务的许多开发测试。支撑系统的机械设计主要由来自火星上的工作环境的独特要求,从陆地甲板的部署和表面上机械分离操作。将解释仪器设计以显示实施哪些设计元素以确保正常功能。必须在支持系统结构开发期间进行各种开发测试。除了标准资格测试,特别QUALIFI

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

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