REG NASA-LLIS-1514--2005 Lessons Learned - One Environmental Effect Can Greatly Complicate Solution of Another.pdf

上传人:confusegate185 文档编号:1019152 上传时间:2019-03-21 格式:PDF 页数:2 大小:13.10KB
下载 相关 举报
REG NASA-LLIS-1514--2005 Lessons Learned - One Environmental Effect Can Greatly Complicate Solution of Another.pdf_第1页
第1页 / 共2页
REG NASA-LLIS-1514--2005 Lessons Learned - One Environmental Effect Can Greatly Complicate Solution of Another.pdf_第2页
第2页 / 共2页
亲,该文档总共2页,全部预览完了,如果喜欢就下载吧!
资源描述

1、Lessons Learned Entry: 1514Lesson Info:a71 Lesson Number: 1514a71 Lesson Date: 2005-02-08a71 Submitting Organization: MSFCa71 Submitted by: William W. Vaughan, Ph.D.Subject: One Environmental Effect Can Greatly Complicate Solution of Another Abstract: For the Chandra thermal-plasma environments inte

2、ractions, the 1992 Program re-baseline removed two instruments, one of which required active thermal control. The orbit for Chandra was changed from LEO to high elliptical and the thermal control concept simplified to passive “cold biased“ surface plus heaters. This change in thermal control concept

3、 resulted in the mandating of silver Teflon thermal control surfaces.Description of Driving Event: The Teflon thermal control surfaces plus the high elliptical orbit resulted in severe spacecraft charging and electrostatic discharge environment, which necessitated an aggressive Electrostatic Dischar

4、ge (ESD) test and circuit protection effort at a cost of over one million dollars.Lesson(s) Learned: Design solutions for one environment effect can greatly complicate solution for change in design as result of Program re-baseline action. Be wary of orbit modifications relative to change in natural

5、environment effects on spacecraft and instruments.Recommendation(s): All orbit modifications for a Program should ensure that effect on the spacecraft and instruments by the change in natural environments are taken into account before a final decision is made. Evidence of Recurrence Control Effectiv

6、eness: Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-N/ADocuments Related to Lesson: NASA-HDBK-1001Mission Directorate(s): a71 Exploration Systemsa71 Space Operationsa71 Aeronautics ResearchAdditional Key Phrase(s): a71 Accident Investigationa71 Co

7、nfiguration Managementa71 Environmenta71 Extra-Vehicular Activitya71 Flight Equipmenta71 Hardwarea71 Mishap Reportinga71 NASA Standardsa71 Parts Materials & Processesa71 Payloadsa71 Policy & Planninga71 Program and Project Managementa71 Risk Management/Assessmenta71 Safety & Mission Assurancea71 Spacecrafta71 Standarda71 Test & VerificationAdditional Info: Approval Info: a71 Approval Date: 2005-04-14a71 Approval Name: Lisa Carra71 Approval Organization: MSFCa71 Approval Phone Number: 256-544-2544Provided 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 2040-1976 Rectangular Steel Bars - Rolled Dimensions - Tolerance js 16 Aerospace Series Edition 1《航空航天系列.长方形钢筋轧后尺寸容差js16.第1版》.pdf AECMA PREN 2040-1976 Rectangular Steel Bars - Rolled Dimensions - Tolerance js 16 Aerospace Series Edition 1《航空航天系列.长方形钢筋轧后尺寸容差js16.第1版》.pdf
  • AECMA PREN 2041-1976 Square Steel Bars - Drawn Dimensions - Tolerances h 11 h 12 Aerospace Series Edition 1《航空航天系列.正方形钢筋冷拉后尺寸容差h 11和h 12.第1版》.pdf AECMA PREN 2041-1976 Square Steel Bars - Drawn Dimensions - Tolerances h 11 h 12 Aerospace Series Edition 1《航空航天系列.正方形钢筋冷拉后尺寸容差h 11和h 12.第1版》.pdf
  • AECMA PREN 2042-1976 Square Steel Bars - Rolled Dimensions - Tolerance js 16 Aerospace Series Edition 1《航空航天系列.正方形钢筋轧后尺寸容差js 16.第1版》.pdf AECMA PREN 2042-1976 Square Steel Bars - Rolled Dimensions - Tolerance js 16 Aerospace Series Edition 1《航空航天系列.正方形钢筋轧后尺寸容差js 16.第1版》.pdf
  • AECMA PREN 2043-1996 Aerospace Series Metallic Materials General Requirements for Semi-Finished Product Qualification (Excluding Forgings and Castings) Edition P 1《航空航天系列.金属材料半成品质量.pdf AECMA PREN 2043-1996 Aerospace Series Metallic Materials General Requirements for Semi-Finished Product Qualification (Excluding Forgings and Castings) Edition P 1《航空航天系列.金属材料半成品质量.pdf
  • AECMA PREN 2044-2000 Aerospace Series Round Bars Drawn in Aluminium and Aluminium Alloys Tolerance Class H 11 Diameter 4 mm Less Than or Equal to D Less Than or Equal to 63 mm Dime.pdf AECMA PREN 2044-2000 Aerospace Series Round Bars Drawn in Aluminium and Aluminium Alloys Tolerance Class H 11 Diameter 4 mm Less Than or Equal to D Less Than or Equal to 63 mm Dime.pdf
  • AECMA PREN 2045-1976 Square Aluminium Alloy Bars - Drawn Dimensions - Tolerance h 11 Aerospace Series Edition 1《航空航天系列.冷拉后正方形铝合金棒材尺寸容差h11.第1版》.pdf AECMA PREN 2045-1976 Square Aluminium Alloy Bars - Drawn Dimensions - Tolerance h 11 Aerospace Series Edition 1《航空航天系列.冷拉后正方形铝合金棒材尺寸容差h11.第1版》.pdf
  • AECMA PREN 2046-1976 Hexagonal Aluminium Alloy Bars - Drawn Dimensions - Tolerance h 11 Aerospace Series Edition 1《航空航天系列.冷拉后六角形铝合金棒材尺寸容差h11.第1版》.pdf AECMA PREN 2046-1976 Hexagonal Aluminium Alloy Bars - Drawn Dimensions - Tolerance h 11 Aerospace Series Edition 1《航空航天系列.冷拉后六角形铝合金棒材尺寸容差h11.第1版》.pdf
  • AECMA PREN 2047-2001 Aerospace Series Beaded L-Section Extruded in Aluminium Alloys Dimensions Editon P 2 Supersedes Edition P 1 August 2000 Replaced by EN 2047《航空航天系列.铝合金冷拉挤压L型材.P.pdf AECMA PREN 2047-2001 Aerospace Series Beaded L-Section Extruded in Aluminium Alloys Dimensions Editon P 2 Supersedes Edition P 1 August 2000 Replaced by EN 2047《航空航天系列.铝合金冷拉挤压L型材.P.pdf
  • AECMA PREN 2048-2001 Aerospace Series Extruded L-Section in Aluminium Alloys Dimensions Edition P 2 Supersedes Edition P 1 August 2000 [Replaced By CEN EN 2048]《航空航天系列.铝合金冷拉挤压L型材.P.pdf AECMA PREN 2048-2001 Aerospace Series Extruded L-Section in Aluminium Alloys Dimensions Edition P 2 Supersedes Edition P 1 August 2000 [Replaced By CEN EN 2048]《航空航天系列.铝合金冷拉挤压L型材.P.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