1. AMP – SAMS/MAMS/PIMS 1 GRC Project Manager: MSI/Kevin McPherson Chief Engineer: Alan Linne Safety Mission Assurance Lead: Bipin Patel NASA Customer: SOMD/Brad Carpenter, JSC ISS Structures and Mechanisms Key Contractor(s): ZIN Technologies Inc. ZIN Task Lead: Jennifer Keller Project Mission Statement: Acceleration Measurement Program will measure, process, analyze, and interpret the ISS acceleration environment as measured by SAMS and MAMS for research payloads and vehicle customers GRC Scope: Planning and operation functions for the SAMS and MAMS acceleration measurement payloads Acceleration data analysis and dissemination for microgravity Principal Investigators Sustaining engineering functions for the SAMS and MAMS acceleration measurement flight systems and associated ground equipment Project Life Cycle Schedule MilestonesSCRHCRPDRCDRVRRSafetyFHALaunchOpsReturnFinal Report Actual/ BaselineN/A 12/19959/19971/20009/200012/20004/2001Inc. 1 ->N/A SAMS Interim Control Unit MAMS Front Panel SAMS acceleration data

2. 2 AMP – SAMS/MAMS/PIMS Project Manager: MSI/Kevin McPherson  Status  Variances Cost – 21% under Year To Date plan Schedule – on schedule, supporting real time ops Technical – no issues Management Key Issue/ConcernPotential ImpactAction Plan Resolution Date TSH-ES S/N08 RepairMSG science support1.Waiting on PFAR final approval. Initial DO modification to fix TSH-ES S/N08 2.Test plan has been completed for TSH-ES and cables 6/2012 Loss of cable from 44PMSG/ESA support1.Effort will begin when budget allows7/2012 CostScheduleTechnicalMgmt. Current MonthGGGG Prior MonthGGGG  Key Issues WBS 904211.04.02.30.01 WBS 401769.06.03.02.02.18

3. 3 AMP – SAMS/MAMS/PIMS Project Manager: MSI/Kevin McPherson  Key Accomplishments SAMS RTS-SE SN 121F02 installed on the SAMS Seat Track Device continues supporting Microgravity Science Glovebox (MSG) science operations Troubleshooting procedure for SAMS TSH-ES sensor SN 08 has been completed. Root cause is an undersized capacitor on a power converter card. Recovery steps are well understood and documented in SAMS-MEM-093 The checkout of the cables SN 01 and SN 03 indicates no problems with the cables. Presented SAMS Control Unit upgrade plan to JSC Vehicle Control board – 5/7/2012. Presented SAMS Control Unit upgrade plan to the Space Station Program Control Board (SSPCB) – 5/16/2012 Presented the following at CSA Event 16 th Canadian Aeronautics and Space Institute (CASI) Astronautics Conference 2012  The NASA Glenn Research Center’s Acceleration Measurement and Analysis Projects' Support for the International Space Station  Key Issues Complete re-certification of SAMS RTS-ES sensor S/N 08 per SAMS-MEM-093 WBS 904211.04.02.30.01 WBS 401769.06.03.02.02.18

4. AMP – SAMS/MAMS/PIMS Milestone Summary Next Milestone Risk None Milestone History (FY11) BaselineProjectedActualSchedule Variance Troubleshoot TSH-ES SN08Dec 11March 12April 12Plan needs PFAR board approval prior to execution. Re-certify TSH-ES SN08 and cables for return to the ISS Feb 2012April 2012Re-certification will be per SAMS-MEM-#### Project Life Cycle Schedule Project is less than 1 month behind planProject is less than 2 months behind planProject is greater than 2 months behind plan Schedule Color Key MilestonesSCRHCRPDRCDRVRRSafetyFHALaunchOpsReturnFinal Report Actual/ BaselineN/A 12/19959/19971/20009/200012/20004/2001Inc. 1 ->N/A WBS 904211.04.02.30.01 WBS 401769.06.03.02.02.18

5. 5 AMP – SAMS/MAMS/PIMS Key Project Metrics AMP in operational mode 100% measurement availability when ISS resources allow SAMS and MAMS equipment to be powered Utilization of SAMS Seat Track Device in US Laboratory in support of MSG. This replaces the function of the failed sensor TSH ES SN 08. Second seat track is deployed in the Columbus module on ER#3 WBS 904211.04.02.30.01 WBS 401769.06.03.02.02.18

6. 6 Project Manager’s Top Challenges 1.Re-qualification and re-flight of the SAMS RTS-ES Sensor S/N 08 and its cabling. 2.Build and re-flight of SAMS cable (P/N 60005E12303, S/N EA12303-02) due to Progress 44P failure 3.SAMS and MAMS completion of 10 years of on-orbit life (April 2001-April 2011). 4.SAMS Control Unit still operating using IBM 760 laptop (considering using new ISS laptop). 5.Likely OZ approval of SAMS ICU replacement. Received approval at PECP on February 6, 2012 for a laptop independent solution. Presenting at the pre-VCB on February 16, 2012, seeking the same approval. Approval received at VCB on May 7, 2012. NOT approved at SSPCB on May 16, 2012 6.1 of 4 ICU temperature sensors exhibiting inconsistent behavior. This issue has not occurred for a while, but still warrants observation and attention. 7.SAMS RTS drawer #2 fan speed regulator issues. 8.Completion of all ground displays for SAMS-ES technology (CIR, FIR, MSG sensors), in particular acceleration versus time interval average and interval minimum/maximum plot types. WBS 904211.04.02.30.01 WBS 401769.06.03.02.02.18

7. Backup Charts 7 Back-up charts will not be briefed unless specifically requested. WBS 904211.04.02.30.01 WBS 401769.06.03.02.02.18

8. AMP – SAMS/MAMS/PIMS Risk Assessment 8 WBS 904211.04.02.30.01 WBS 401769.06.03.02.02.18