REG NASA-LLIS-1484--2004 Lessons Learned The Mission Operational Design Should Allow for Down Days (2004).pdf

上传人:boatfragile160 文档编号:1019122 上传时间:2019-03-21 格式:PDF 页数:3 大小:15.25KB
下载 相关 举报
REG NASA-LLIS-1484--2004 Lessons Learned The Mission Operational Design Should Allow for Down Days  (2004).pdf_第1页
第1页 / 共3页
REG NASA-LLIS-1484--2004 Lessons Learned The Mission Operational Design Should Allow for Down Days  (2004).pdf_第2页
第2页 / 共3页
REG NASA-LLIS-1484--2004 Lessons Learned The Mission Operational Design Should Allow for Down Days  (2004).pdf_第3页
第3页 / 共3页
亲,该文档总共3页,全部预览完了,如果喜欢就下载吧!
资源描述

1、Lessons Learned Entry: 1484Lesson Info:a71 Lesson Number: 1484a71 Lesson Date: 2004-08-02a71 Submitting Organization: JPLa71 Submitted by: Mark Boyles, David OberhettingerSubject: The Mission Operational Design Should Allow for “Down Days“ (2004) Abstract: Early in the Mars Exploration Rover (MER) d

2、esign phase, and in all modeling for operations and mission science return, planners assumed that each rover would be inoperable every third day, on average, due to problems. This planned margin contributed to mission success by giving operations personnel time to gain an understanding of problems,

3、and to plan high-risk maneuvers, before taking action. For complex missions, provide sufficient margin in the planned mission science return to accommodate likely interruptions in the data flow.Description of Driving Event: Early in the Mars Exploration Rover (MER) design phase, and in all modeling

4、for operations and mission science return, planners assumed that each rover would be inoperable every third day, on average, due to problems. MERs daily command cycle and 90-day prime mission lifetime requirement were factors in deciding to make this assumption. The benefit of making allowances for

5、these hypothetical “down days” was that it provided: 1. Enough margin in the planned mission return to accommodate losses such as the roughly two-week data loss due to the Spirit flash memory problem, and2. A benchmark against which to compare actual lost days of operation. This helped JPL to determ

6、ine whether it was on track to meet mission and science return criteria and contributed to meeting full mission success.This mission design assumption enabled a cautious approach during surface operations when responding to detection of anomalies and when planning the execution of high-risk maneuver

7、s by the MER operations team. Spirit, the first of the two MER rovers, was delayed in its “drive-off” of the lander when airbags hampered the preferred egress path (Figure 1). Later, Spirit experienced a Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-

8、problem with its flash memory for 2 weeks. The operations team for the second rover, Opportunity, spent several days determining the safety of entering the crater Endurance. During these and other surface mission events, operations personnel were not under undue pressure to return to science opera

9、tions, but instead took sufficient time to gain confidence in their understanding of the situation before taking action. refer to D descriptionDAdditional Key Words: operational margin, operations margin, mission planning, operations design Lesson(s) Learned: For complex spaceflight missions, it is

10、very likely that unforeseen factors will cause interruptions in the science data return. Recommendation(s): For complex missions such as landers or rovers, provide sufficient margin in mission return/success operational scenarios to accommodate likely interruptions in the data flow on the order of s

11、everal days. Such margin may be on the order of 30% or more depending on the complexity of the mission. Evidence of Recurrence Control Effectiveness: Corrective Action Notice No. Z85350 was opened by JPL on January 4, 2005 to initiate and document appropriate Laboratory-wide corrective action on the

12、 above recommendation.Documents Related to Lesson: Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-N/AMission Directorate(s): a71 ScienceAdditional Key Phrase(s): a71 Flight Operationsa71 Hardwarea71 Payloadsa71 Policy & Planninga71 Risk Management/A

13、ssessmenta71 Safety & Mission Assurancea71 SpacecraftAdditional Info: Approval Info: a71 Approval Date: 2004-09-22a71 Approval Name: Carol Dumaina71 Approval Organization: JPLa71 Approval Phone Number: 818-354-8242Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-

展开阅读全文
相关资源
猜你喜欢
  • EN 1822-3-2009 en High efficiency air filters (EPA HEPA and ULPA) - Part 3 Testing flat sheet filter media《高效空气过滤器(HEPA和ULPA) 第3部分 试验扁平片状过滤介质》.pdf EN 1822-3-2009 en High efficiency air filters (EPA HEPA and ULPA) - Part 3 Testing flat sheet filter media《高效空气过滤器(HEPA和ULPA) 第3部分 试验扁平片状过滤介质》.pdf
  • EN 1822-4-2009 en High efficiency air filters (EPA HEPA and ULPA) - Part 4 Determining leakage of filter elements (scan method)《高效空气过滤器(EPA HEPA和ULPA) 第4部分 过滤元件泄漏性测定(扫描法)》.pdf EN 1822-4-2009 en High efficiency air filters (EPA HEPA and ULPA) - Part 4 Determining leakage of filter elements (scan method)《高效空气过滤器(EPA HEPA和ULPA) 第4部分 过滤元件泄漏性测定(扫描法)》.pdf
  • EN 1822-5-2009 en High efficiency air filters (EPA HEPA and ULPA) - Part 5 Determining the efficiency of filter elements《高效空气过滤器(HEPA和ULPA) 第5部分 过滤元件效率测定》.pdf EN 1822-5-2009 en High efficiency air filters (EPA HEPA and ULPA) - Part 5 Determining the efficiency of filter elements《高效空气过滤器(HEPA和ULPA) 第5部分 过滤元件效率测定》.pdf
  • EN 1824-2011 en Road marking materials - Road trials《道路标记材料 道路试验》.pdf EN 1824-2011 en Road marking materials - Road trials《道路标记材料 道路试验》.pdf
  • EN 1825-1-2004 en Grease separators - Part 1 Principles of design performance and testing marking and quality control《油脂分离器 第1部分 设计 性能和试验以及标记和质量控制的准则》.pdf EN 1825-1-2004 en Grease separators - Part 1 Principles of design performance and testing marking and quality control《油脂分离器 第1部分 设计 性能和试验以及标记和质量控制的准则》.pdf
  • EN 1825-2-2002 en Grease Separators - Part 2 Selection of Nominal Size Installation Operation and Maintenance《油脂分离器 第2部分 标称尺寸的选择 安装 操作和维修》.pdf EN 1825-2-2002 en Grease Separators - Part 2 Selection of Nominal Size Installation Operation and Maintenance《油脂分离器 第2部分 标称尺寸的选择 安装 操作和维修》.pdf
  • EN 1826-1996 en Biotechnology - Large-Scale Process and Production - Control Procedures for Raw Materials《生物工艺学 大比例方法和生产 原材料监督控制方法》.pdf EN 1826-1996 en Biotechnology - Large-Scale Process and Production - Control Procedures for Raw Materials《生物工艺学 大比例方法和生产 原材料监督控制方法》.pdf
  • EN 1827-1999 en Respiratory protective devices - Half masks without inhalation valves and with separable filters to protect against gases or gases and particles or particles only -.pdf EN 1827-1999 en Respiratory protective devices - Half masks without inhalation valves and with separable filters to protect against gases or gases and particles or particles only -.pdf
  • EN 1829-1-2010 en High pressure water jet machines - Safety requirements - Part 1 Machines《高压喷水机械 安全要求 第1部分 机械》.pdf EN 1829-1-2010 en High pressure water jet machines - Safety requirements - Part 1 Machines《高压喷水机械 安全要求 第1部分 机械》.pdf
  • 相关搜索

    当前位置:首页 > 标准规范 > 国际标准 > 其他

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1