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AMS-02 QUALITY SYSTEM, CONFIGURATION MANAGEMENT OVERVIEW AND AMS WEBSITE

AMS-02 QUALITY SYSTEM, CONFIGURATION MANAGEMENT OVERVIEW AND AMS WEBSITE. AMS QUALITY SYSTEM, CONFIGURATION MANAGEMENT OVERVIEW, AND AMS WEBSITE. AMS QUALITY SYSTEM MIKE FOHEY CONFIGURATION MANAGEMENT PLAN MIKE FOHEY LMSO QUALITY SYSTEM &

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AMS-02 QUALITY SYSTEM, CONFIGURATION MANAGEMENT OVERVIEW AND AMS WEBSITE

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  1. AMS-02 QUALITY SYSTEM, CONFIGURATION MANAGEMENT OVERVIEW AND AMS WEBSITE

  2. AMS QUALITY SYSTEM, CONFIGURATION MANAGEMENT OVERVIEW, AND AMS WEBSITE AMS QUALITY SYSTEM MIKE FOHEY CONFIGURATION MANAGEMENT PLAN MIKE FOHEY LMSO QUALITY SYSTEM & CONFIGURATION MANAGEMENT DAVE ELMORE SAFETY & MISSION ASSURANCE PLAN DAVID KAPLAN EXPERIMENT MILESTONE LOG CHRIS TUTT JSC AMS WEBSITE MIKE FOHEY

  3. ALPHA MAGNETIC SPECTROMETER – 02 (AMS-02) QUALITY SYSTEMS Mike Fohey July 15, 2004

  4. AMS QUALITY SYSTEMS • The Quality Management System (QMS) for JSC onsite design, development, and manufacturing shall be in accordance with JPD 5335.1, JSC Quality Policy and Quality Manual. • For offsite Lockheed Martin Space Operations (LMSO) activities (including procurements) the QMS shall conform to LMSEAT-31041, Quality System Manual (QSM) for the Science, Engineering, Analysis, and Test (SEAT) Operation. • The AMS Collaboration is responsible for selecting their own QMS. A QMS consistent with ISO 9001-2000 requirements is recommended.

  5. ALPHA MAGNETIC SPECTROMETER – 02 (AMS-02) CONFIGURATION MANAGEMENT PLAN Mike Fohey July 15, 2004

  6. PURPOSE • The CMP ensures that: • Programmatic commitments are met • Shuttle/Space Station-to-AMS Payload and Experiment-to-AMS Payload Integration Hardware (PIH) compatibility is achieved • Proposed AMS Experiment and Payload interface changes are processed and dispositioned in a formal and coordinated manner

  7. SCOPE • The CMP encompasses the management of: • Design Requirements • Specifications • Critical Milestones • Interface Agreements • Flight Hardware Mission Requirements

  8. SCOPE • The CMP specifically addresses the configuration control of the AMS interfaces to the Shuttle and Space Station • The CMP does not address the internal AMS Experiment configuration.

  9. CONFIGURATION CONTROL BOARD • The CMP establishes a Configuration Control Board (CCB) as the controlling authority for: • Establishing the initial AMS project-level baseline • Making changes to the baseline (when required) • Controlling the AMS project-level documents and drawings • Reviewing and dispositioning AMS generated change requests

  10. CONFIGURATION CONTROL BOARD

  11. MEETING SCHEDULE • There will be weekly AMS Status Meetings on Tuesdays from 9:00 – 10:00 AM beginning August 3, 2004. The preliminary standard agenda includes: Risk Management Plan updates, status reports from LMSO and the Collaboration, and a review ofproject milestones. • The first Tuesday meeting of each month will be reserved for the AMS CCB. (NOTE: The meeting on August 3rd may or may not be a CCB.)

  12. CONTROLLED CLASSES* & IDENTIFICATION • The CMP establishes Configuration Control for all AMS GFE hardware, software and firmware that is Class I (Flight), Class II (controlled Non-flight), Class IIIW (controlled Non-flight), and GSE* • The CMP defines the requirements for configuration identification of all controlled hardware, software and firmware * See CMP for definitions of Hardware Classifications

  13. Requirements contained in the AMS Baseline Contract cost/provisions Interchangeability Safety Interfaces Any change to baselined documentation under configuration control Corrections to drawing errors “As-built” changes (i.e. does not affect fit, form, or function) to hardware which do not affect Class I items Additions of “either/or” items giving such choices as color preference CHANGE DEFINITIONS Type I Changes Type II Changes • Type I Changes to baselined hardware, software, firmware, drawings, and AMS baselined documents shall be submitted to and approved by the CCB prior to implementation. • Type II Changes do not require CCB approval.

  14. CHANGE REQUEST PROCEDURES • Detailed procedures for preparing and submitting AMS Change Requests can be found in JSC 27542, Alpha Magnetic Spectrometer – 02 (AMS-02) Configuration Management Plan

  15. ALPHA MAGNETIC SPECTROMETER – 02 (AMS-02) SAFETY AND MISSION ASSURANCE PLAN David Kaplan July 15, 2004

  16. ALPHA MAGNETIC SPECTROMETER – 02 (AMS-02) EXPERIMENT MILESTONE LOG Chris Tutt July 15, 2004

  17. Experiment Milestone Log • Experiment Milestone Log will contain key verification and integration milestones for the experiment hardware. • Goal is to give NASA project management insight into experiment status, not control. • Log will be maintained by LMSO and status reported monthly at AMS CCB.

  18. Sample Log Items • Non-safety related test dates and status for experiment hardware. • Functional tests • Non-safety structural and thermal tests • Major integration milestone dates for collaboration hardware. • Manufacturing schedules for collaboration hardware. • Certification of Compliance status for major hardware items.

  19. Experiment Milestone Log Status • Milestone log still in early development. • LMSO will meet with collaboration at next quarterly TIM and begin selecting appropriate milestones. • Final selection of what will be tracked will be made jointly by AMS collaboration and NASA/JSC.

  20. ALPHA MAGNETIC SPECTROMETER – 02 (AMS-02) ENGINEERING DIRECTORATE (EA) WEBSITE Mike Fohey July 15, 2004

  21. AMS-02 EA WEBSITE • The proposed solution to allow all of the AMS Project Team access to the website is to move all of the non-controlled documentation to a “green” server. • A “green” server is open for public access as opposed to the current “amber” server that is open to users on the JSC domain (JSC, contractors, and other NASA sites). • To facilitate configuration management, both the internal and external web pages will access files that reside on the external server.

  22. AMS-02 EA WEBSITE – JSC INTERNAL • The URL for the AMS Internal Website is: • The internal website gives users in the JSC domain the ability to use the links on the left side of the page to access locations inside the JSC firewall. • The internal website gives users access to the AMS RID System and the AMS Risk Management System. http://www4.jsc.nasa.gov/eaprojects/ea-projects/flightgfe/ams_02/html/ams_02.htm

  23. AMS-02 EA WEBSITE – JSC INTERNAL

  24. AMS-02 EA WEBSITE – EXTERNAL • The URL for the AMS External Website is TBD. A “green” server with available space needs to be located. • A potential work-around for the Risk Management System would be to modify the AMS Risk Management Application link to point to an overview report that provides a status of the risks. • Members of the AMS Project Team that do not have access to the Internal Website will submit RIDs using RID forms and they will be entered into the RID System for them.

  25. AMS-02 EA WEBSITE – EXTERNAL

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