REG NASA-LLIS-1466-2003 Lessons Learned Accident Investigations Software Tool Selection.pdf

上传人:刘芸 文档编号:1019104 上传时间:2019-03-21 格式:PDF 页数:3 大小:14.62KB
下载 相关 举报
REG NASA-LLIS-1466-2003 Lessons Learned Accident Investigations Software Tool Selection.pdf_第1页
第1页 / 共3页
REG NASA-LLIS-1466-2003 Lessons Learned Accident Investigations Software Tool Selection.pdf_第2页
第2页 / 共3页
REG NASA-LLIS-1466-2003 Lessons Learned Accident Investigations Software Tool Selection.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: 1466Lesson Info:a71 Lesson Number: 1466a71 Lesson Date: 2003-08-31a71 Submitting Organization: JSCa71 Submitted by: David LengyelSubject: Accident Investigations/Software Tool Selection Abstract: Difficulties with the single software tool selected to support the Columbia accid

2、ent investigation point to a need for a functional requirements analysis by a team experienced in the IT requirements of a large-scale mishap investigation prior to tool selection.Description of Driving Event: The main driver for software tool selection to support the Columbia Accident Investigation

3、 Board (CAIB) was the requirement for a single tool with remote access capability and strong security to protect sensitive mishap investigation data. Without defining a clear set of functional requirements in advance, one tool was chosen to be all things to all people collaborative environment (i.e.

4、 portal for group calendar & file sharing, announcements, links, etc.), action tracking database, library management, data archive). As a result, after significant start up investment was made to get off the ground with the selected tool, subsequent unidentified requirements required custom softwar

5、e engineering, causing delays in functional capability and frustrations for investigation staff members. In addition, the selected tool was set up in an untested environment involving additional layers of network security that interfered with the normal operation of the tool and complicated/delayed

6、fixing problems that arose.Lesson(s) Learned: A functional requirements analysis should be performed prior to software tool selection, and this analysis needs to be performed by a team of people experienced in the IT requirements of a large-scale mishap investigation. In addition, clear IT security

7、requirements need to be identified in advance of tool selection to ensure appropriate safeguarding of sensitive data.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Recommendation(s): a71 Integrate a set of individual tools into a CAP system that is

8、vetted and available prior to the start of the investigation. Widespread, long-term buy-in and use by the investigation and support teams of a single on-line software solution for configuration management, electronic library capability, action tracking database, and document search & retrieval may n

9、ot be attainable.a71 Avoid tools that would not be familiar to investigation staff ahead of time, or tools that would be overly complex requiring steep learning curves. The tools should be easy to use and easy to learn. By vetting the CAP system of tools in advance, problems with IT availability, ac

10、cess control, and security issues can be avoided. Evidence of Recurrence Control Effectiveness: TBD NASA ResponseDocuments Related to Lesson: Agency Contingency Action Plan for Space Flight OperationsMission Directorate(s): a71 Space Operationsa71 Exploration SystemsAdditional Key Phrase(s): a71 Acc

11、ident Investigationa71 Administration/Organizationa71 Computersa71 Configuration Managementa71 Information Technology/Systemsa71 NASA Standardsa71 Policy & Planninga71 Safety & Mission Assurancea71 SecurityAdditional Info: Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Approval Info: a71 Approval Date: 2004-06-16a71 Approval Name: Ronald Montaguea71 Approval Organization: JSCa71 Approval Phone Number: 281-483-8576Provided 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
  • AECMA PREN 2607-1987 Aerospace Series Straight Metric-Size Unions with Locking Ring Configuration O-Ring Dimensions Issue P 1《航空航天系列公制尺寸直管活结O-形锁紧环尺寸》.pdf AECMA PREN 2607-1987 Aerospace Series Straight Metric-Size Unions with Locking Ring Configuration O-Ring Dimensions Issue P 1《航空航天系列公制尺寸直管活结O-形锁紧环尺寸》.pdf
  • AECMA PREN 2608-1999 Aerospace Series Installation and Removal Requirements for 8 Degree 30' Adaptors Threaded with Lockring Edition P 1《航空航天系列带锁环的8°、30'螺纹适配器的锁环安装和移除要求》.pdf AECMA PREN 2608-1999 Aerospace Series Installation and Removal Requirements for 8 Degree 30' Adaptors Threaded with Lockring Edition P 1《航空航天系列带锁环的8°、30'螺纹适配器的锁环安装和移除要求》.pdf
  • AECMA PREN 2609-1985 Aerospace Series Turnbarrels Control Cable in Copper-Zinc Alloys Dimensions and Loads Edition 1《航空航天系列操纵缆绳用铜锌合金套筒尺寸和荷载》.pdf AECMA PREN 2609-1985 Aerospace Series Turnbarrels Control Cable in Copper-Zinc Alloys Dimensions and Loads Edition 1《航空航天系列操纵缆绳用铜锌合金套筒尺寸和荷载》.pdf
  • AECMA PREN 2615-1986 Aerospace Series Wire to Close Tolerance in Aluminium and Aluminium Alloys 1 6 Less Than or Equal to D Less Than or Equal to 9 6 mm Dimensions Issue P 1《航空航天系列.pdf AECMA PREN 2615-1986 Aerospace Series Wire to Close Tolerance in Aluminium and Aluminium Alloys 1 6 Less Than or Equal to D Less Than or Equal to 9 6 mm Dimensions Issue P 1《航空航天系列.pdf
  • AECMA PREN 2616-1986 Aerospace Series Wire for Rivets in Aluminium and Aluminium Alloys Large Tolerances D Less Than or Equal to 10 mm Dimensions Issue P 1《航空航天系列铝及铝合金柳钉线材尺寸最大允许偏差直.pdf AECMA PREN 2616-1986 Aerospace Series Wire for Rivets in Aluminium and Aluminium Alloys Large Tolerances D Less Than or Equal to 10 mm Dimensions Issue P 1《航空航天系列铝及铝合金柳钉线材尺寸最大允许偏差直.pdf
  • AECMA PREN 2617-1995 Aerospace Series Plate in Titanium and Titanium Alloys Thickness 6 mm Less Than a Less Than or Equal to 100 mm Dimensions Edition P 2《航空航天系列钛和钛合金板5小于或等于100mm 尺.pdf AECMA PREN 2617-1995 Aerospace Series Plate in Titanium and Titanium Alloys Thickness 6 mm Less Than a Less Than or Equal to 100 mm Dimensions Edition P 2《航空航天系列钛和钛合金板5小于或等于100mm 尺.pdf
  • AECMA PREN 2621-1986 Aerospace Series Circular Structural Tubes Seamless in Low Alloy Steel 4 Less Than or Equal to D Less Than or Equal to 100 mm 0 5 Less Than or Equal to a Less .pdf AECMA PREN 2621-1986 Aerospace Series Circular Structural Tubes Seamless in Low Alloy Steel 4 Less Than or Equal to D Less Than or Equal to 100 mm 0 5 Less Than or Equal to a Less .pdf
  • AECMA PREN 2622-1996 Aerospace Series Circular Tube for Fluids in Heat Resisting Alloys Diameter 3 2 mm Less Than or Equal to D Less Than or Equal to 100 mm Thickness 0 32 mm Less D.pdf AECMA PREN 2622-1996 Aerospace Series Circular Tube for Fluids in Heat Resisting Alloys Diameter 3 2 mm Less Than or Equal to D Less Than or Equal to 100 mm Thickness 0 32 mm Less D.pdf
  • AECMA PREN 2623-1986 Aerospace Series Electrical Cables for General Purpose Operating Temperatures between - 55 Degrees Celsius and + 135 Degrees Celsius Issue P 1《航空航天系列通用电缆操作温度 负.pdf AECMA PREN 2623-1986 Aerospace Series Electrical Cables for General Purpose Operating Temperatures between - 55 Degrees Celsius and + 135 Degrees Celsius Issue P 1《航空航天系列通用电缆操作温度 负.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