REG NASA-LLIS-4770-2010 Lessons Learned - Recurring Flight Project Problems Evince Common Threads .pdf

上传人:outsidejudge265 文档编号:1019464 上传时间:2019-03-21 格式:PDF 页数:4 大小:73.49KB
下载 相关 举报
REG NASA-LLIS-4770-2010 Lessons Learned - Recurring Flight Project Problems Evince Common Threads .pdf_第1页
第1页 / 共4页
REG NASA-LLIS-4770-2010 Lessons Learned - Recurring Flight Project Problems Evince Common Threads .pdf_第2页
第2页 / 共4页
REG NASA-LLIS-4770-2010 Lessons Learned - Recurring Flight Project Problems Evince Common Threads .pdf_第3页
第3页 / 共4页
REG NASA-LLIS-4770-2010 Lessons Learned - Recurring Flight Project Problems Evince Common Threads .pdf_第4页
第4页 / 共4页
亲,该文档总共4页,全部预览完了,如果喜欢就下载吧!
资源描述

1、 Public Lessons Learned Entry: 4770 Lesson Info: Lesson Number: 4770 Submitting Organization: JPL Submitted by: David Oberhettinger Subject: Recurring Flight Project Problems Evince “Common Threads“ Abstract: A Common Threads Workshop was held by JPL in 1996 and 1997 as a venue for seasoned flight p

2、roject managers to convey knowledge of recurring problems or situations that dominate the project life cycle to future project leaders. Most of these issues appear relevant today. The workshop summary reports suggest “corrective strategies“ for coping with “common thread“ issues that arise on projec

3、t after project. Description of Driving Event: JPL held a Common Threads Workshop in May 1996 and again in July 1997 as a venue for seasoned flight project managers (PMs) to convey some key knowledge to the next generation of PMs. The premise in organizing the workshops was that “common threads“ exi

4、st that are evident in project after project, in the form of similar flight and test failures or failure mechanisms, programmatic issues, and sometimes serious oversights. These problems are well understood and often solved in some innovative way on one project or program, but the knowledge is frequ

5、ently not passed to another project with a similar problem. Thirteen years after the publication of the workshop reports (References (1) and (2), most of these overriding engineering issues still appear relevant. The workshop presentations consisted of experienced PMs and other JPL engineering leade

6、rs describing issues and coping techniques that arose during their program/project stewardship that gave them a deeper understanding of constraints to mission success. The format of each presentation was either “war stories“ specific to a project or “lessons learned“ from general experience. The 199

7、6 workshop involved mostly PMs focusing on programmatic issues, while the 1997 workshop involved more Engineering and Science Directorate personnel focusing on design issues. The common threads mutual to both workshops fell into the following 8 general categories: Communications issues at all levels

8、 Hardware interfaces Contractual interfaces Heritage and commercial-off-the-shelf (COTS) issues Parts issues Programmatic issues Assembly, Test, and Launch Operations (ATLO) and launch site issues Product assurance issues Within these groupings, there was a high level of agreement between presenters

9、 on specific common threads, such as: “Failure to convey lessons learned from one project to the next and to all project elements, including the contractor and subcontractors“ (a “Communications“ common thread). “Placing too much trust in inherited hardware“ (a “Heritage/COTS“ common thread). “Deter

10、mining the proper amount of burn-in time“ (a “Parts“ common thread). Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-“Growth in science requirements that jeopardize the mission“ (a “Programmatic“ common thread). “Failure to consider the differences i

11、n the test environment and the flight environment“ (an “ATLO“ common thread, often stated as “Test as you fly“). References: 1. Arthur F. Brown and John E. Koch, “JPL Common Threads Workshop Summary Report,“ JPL Document No. D-13776, May 31, 1996. 2. Arthur F. Brown and John E. Koch, “JPL Common Thr

12、eads Workshop II Summary Report,“ JPL Document No. D-14906, July 25, 1997. Lesson(s) Learned: There exist overriding “common thread“ engineering issues that are evident in flight project after flight project, but techniques for coping with recurring constraints to mission success are not always comm

13、unicated to the next generation of PMs. Most of these common threads may not be unique to JPL, but they are all significant to JPL because they are central to its engineering culture. Recommendation(s): Each summary report provides “corrective strategies“ for coping with specific common thread issue

14、s. (There is a 1990s-era emphasis on coping with “Faster-Better-Cheaper“ constraints, particularly in Reference (2), but many of these constraints apply to todays cost-constrained missions.) In addition, the reports provide a set of overall recommendations specific to the general categories of commo

15、n threads: 1. Communications. Work on communications at all levels - i.e., within the project; between the project and such support organizations as product assurance and safety; as well as with the contractor, subcontractor, and fabrication and assembly personnel. Projects must take advantage of le

16、ssons learned and other knowledge that already exists at the Laboratory, though it may require crossing an organizational boundary. 2. Interfaces. Beware of interfaces of all kinds - hardware to hardware; hardware to test and ground support equipment (GSE); spacecraft to launch vehicle; and people t

17、o people. Be especially careful when a system is designed by one group and used by another. 3. Heritage. Evaluate inherited hardware as thoroughly as new hardware. There is a tendency to put too much trust in inherited hardware. Several examples were presented in which the new spacecraft application

18、 presented life or environmental challenges not faced in the original application, and the inherited device failed. 4. Parts. Semiconductor parts are getting more reliable, but NASA and DoD programs have less control than they once did. It is becoming harder to get radiation-hardened parts, and this

19、 presents new challenges such as providing Single Event Effect (SEE) tolerance at the system level. Work with the Parts organization early to prevent delays on long lead items. 5. Programmatic. There is “sales“ pressure for projects to provide extraordinary levels of science and mission complexity w

20、hile staying within severely constrained schedules and budgets, and upper management must be made fully aware of any increased risk. Monitor the fundamental program assumptions, and replan when fundamental assumptions change. Ensure that project reviews are thorough: the major benefit of design revi

21、ews is the time spent preparing for them. 6. ATLO and Launch Site Issues. The workshop consensus on the correct amount of time in ATLO was somewhere between twelve and eighteen months, depending on how well people, parts and processes are understood. The new projects wish ATLO (i.e., Integration & T

22、est) to be flexible enough to add new tests as the knowledge of the hardware increases. Provide time and budget contingencies in ATLO to deal with the unexpected. Ensure that written, well rehearsed, procedures are available before shipping hardware to the Cape. 7. Product Assurance. There is a stro

23、ng relationship between adequate product assurance and successful programs. The PMs favored continuation of the practice of having Mission Assurance (especially Reliability Engineering) personnel collocated with Provided by IHSNot for ResaleNo reproduction or networking permitted without license fro

24、m IHS-,-,-flight project personnel. Evidence of Recurrence Control Effectiveness: There are documented flight project practices that emphasize infusion of lessons learned. However, the theme of this document is that these “common thread“ issues will recur. Documents Related to Lesson: JPL Common Thr

25、eads Workshop Summary Report, 31 May 1996 Click here to download communication document. Mission Directorate(s): Space Operations Science Exploration Systems Aeronautics Research Additional Key Phrase(s): Program Management.Science integration Program Management.Program planning, development, and ma

26、nagement Program Management.Contractor relationships Program Management.Configuration and data management Program Management.Communications between different offices and contractor personnel Missions and Systems Requirements Definition. Missions and Systems Requirements Definition.Configuration cont

27、rol and data management Systems Engineering and Analysis. Mission Operations and Ground Support Systems.Training and simulation systems Mission Operations and Ground Support Systems.Logistics and maintenance Mission Operations and Ground Support Systems.Launch support systems Mission Operations and

28、Ground Support Systems. Integration and Testing Manufacturing and Assembly Engineering Design (Phase C/D).Spacecraft and Spacecraft Instruments Engineering Design (Phase C/D).Software Engineering Engineering Design (Phase C/D). Systems Engineering and Analysis.Engineering design and project processe

29、s and standards Program Management. Safety and Mission Assurance.Configuration Change Control Safety and Mission Assurance.Product Assurance Safety and Mission Assurance.Review systems and boards Additional Categories. Additional Categories.Configuration Management Additional Categories.Energetic Ma

30、terials - Explosive/Propellant/Pyrotechnic Additional Categories.Hardware Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Additional Categories.Parts, Materials, & Processes Additional Categories.Payloads Additional Categories.Procurement, Small Busi

31、ness & Industrial Relations Additional Categories.Safety & Mission Assurance Additional Categories.Test & Verification Safety and Mission Assurance. Additional Info: Project: N/A Approval Info: Approval Date: 2010-12-30 Approval Name: mbell Approval Organization: HQ Provided 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
  • DIN 49441-2-1989 Two-pole plugs with earthing contact rated for 10 A 250 V d c  16 A 250 V a c  splash-proof《额定功率为直流10A 250V和交流16A 250V、带接地接触点防溅型二极插头》.pdf DIN 49441-2-1989 Two-pole plugs with earthing contact rated for 10 A 250 V d c 16 A 250 V a c splash-proof《额定功率为直流10A 250V和交流16A 250V、带接地接触点防溅型二极插头》.pdf
  • DIN 49441-3-1989 Two-pole plugs with earthing contact rated for 10 A 250 V a c  16 A 250 V d c  gauges for checking the outside diameter of plugs test apparatus《额定功率为直流10A 250V和交流1.pdf DIN 49441-3-1989 Two-pole plugs with earthing contact rated for 10 A 250 V a c 16 A 250 V d c gauges for checking the outside diameter of plugs test apparatus《额定功率为直流10A 250V和交流1.pdf
  • DIN 49442-1969 Two-pole watertight socket-outlets with earthing-contact 10 A 250 V and 10 A 250 V 16 A 250 V principal dimensions《交直流250V 10A和直流250V 10A交流250V 16A带接地触点的输出装置的防水两极插座 .pdf DIN 49442-1969 Two-pole watertight socket-outlets with earthing-contact 10 A 250 V and 10 A 250 V 16 A 250 V principal dimensions《交直流250V 10A和直流250V 10A交流250V 16A带接地触点的输出装置的防水两极插座 .pdf
  • DIN 49443-1987 Watertight two-pole plug with earthing contact 10A 250 V d c  16A 250 V a c 《带接地保护触点的防水的两极插头 直流10A 250 V,交流16A 250 V》.pdf DIN 49443-1987 Watertight two-pole plug with earthing contact 10A 250 V d c 16A 250 V a c 《带接地保护触点的防水的两极插头 直流10A 250 V,交流16A 250 V》.pdf
  • DIN 49445-1991 Three-pole socket-outlets with N- and earthing contacts 16 A 400 230 V a c  principal dimensions《带N 触点和接地触点的16A 400 230V交流三极插座 主要尺寸》.pdf DIN 49445-1991 Three-pole socket-outlets with N- and earthing contacts 16 A 400 230 V a c principal dimensions《带N 触点和接地触点的16A 400 230V交流三极插座 主要尺寸》.pdf
  • DIN 49446-1999 Three-pole plug with N- and earthing contacts AC 400 230 V 16 A - Principal dimensions《带N触点和接地触点的16A400 230V交流电用三极插头 主要尺寸》.pdf DIN 49446-1999 Three-pole plug with N- and earthing contacts AC 400 230 V 16 A - Principal dimensions《带N触点和接地触点的16A400 230V交流电用三极插头 主要尺寸》.pdf
  • DIN 49447-1991 Three-pole socket-outlets with N- and earthing contacts 25 A 400 230 V a c  principal dimensions《带N 触点和接地触点的25A 400 230V交流三极插座 主要尺寸》.pdf DIN 49447-1991 Three-pole socket-outlets with N- and earthing contacts 25 A 400 230 V a c principal dimensions《带N 触点和接地触点的25A 400 230V交流三极插座 主要尺寸》.pdf
  • DIN 49448-1991 Three-pole plug with N- and earthing contacts 25 A 400 230 V a c  principal dimensions《带N 触点和接地触点的25A 400 230V交流三极插头 主要尺寸》.pdf DIN 49448-1991 Three-pole plug with N- and earthing contacts 25 A 400 230 V a c principal dimensions《带N 触点和接地触点的25A 400 230V交流三极插头 主要尺寸》.pdf
  • DIN 4945-1-2005 Rising pipes with tension proof socket for water raising - Part 1 Steel pipes DN 50 to DN 200 plastic coated《抽水用带抗拉套管的出水竖管 第1部分:DN 50至 DN 200的塑料涂层钢管》.pdf DIN 4945-1-2005 Rising pipes with tension proof socket for water raising - Part 1 Steel pipes DN 50 to DN 200 plastic coated《抽水用带抗拉套管的出水竖管 第1部分:DN 50至 DN 200的塑料涂层钢管》.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