David Miller

-Performed integrated analysis for external hardware on the space station including the External Logistics Carriers (ELCs), Capture Latch Assemblies (CLAs), and Common Berthing Mechanisms (CBMs). -Lead 2-Fault Analysis for EVAs on final shuttle flights and post shuttle EVAs. Includes directing what hardware needs analysis, incorporating data and experience from previous EVAs and coordinating responses from multiple stakeholders (EVA, EV&CS, Tools, Safety, etc.). -Worked live Ops in the MER for Quiescent Ops, Shuttle Ops, CBM Ops, and EVAs. Including working solutions to immediate issues during EVAs (PSARJ Cover bolt failures during SARJ greasing on ULF-6 EVA2, MBSU Install troubleshooting on Stage EVA18 and EVA19). -Coordinated measurement and performed analysis of CTC-2/TRJJ close clearance. Updated options and presented deltas to boards to ensure compliance as multiple shuttle and other schedule slips ruled out original plan. Our SSRMS Photogrammetry analysis allowed us to clear the potential on-orbit impact hazard. Successfully proposed new flight rules to ensure vehicle operates safely going forward. -Wrote CBM Bolt Torque Trending Tool in Matlab. This tool allowed us to find and analyze peak CBM bolt torques minutes after a berthing rather than the days of the manual process. Reduced touch time for each berthing analysis from 8 hours to 20 minutes.

-Performed physical tests and computational analysis on Intra- and Extra- vehicular cables flown on the Space Station. - Lead audits with 5-20 participants. (Including NASA customer, Crew, Quality, Suppliers etc.) Wrote procedures and reports for all audits. Worked with cable designers, builders, and quality assurance team to resolve Problem Reports and Non-Conformances found during audits. (C&FA audits are the final inspection before handing over flight hardware to the NASA customer). -Performed Cable Audits on equipment flying to the Space Station on STS-128 (Flight 17A), STS-130 (Flight 20A), STS-132 (Flight ULF4), and many post-shuttle cargo missions -Implementing process improvement that will lower work time on each On-Orbit Effects Analysis by 40%.

-Used photogrammetry, laser tracking, and laser scanning to measure and create ultra-high precision CAD models of Space Station nodes and major components. -Worked in Italy for three weeks taking measurements of Node 3 (Tranquility) at the Thales Alenia facility in Turin, Italy. -Successfully aligned ELC1 and ELC2 keels for integration into the Shuttle Payload Bay. -Aligned Cupola for successful ground mate with Node 3. -Measured docking surfaces to ensure success on-orbit for both commercial cargo partners (SpaceX and Orbital) before their respective first missions to the International Space Station.

-Performed kinematic analysis for Space Station and Space Shuttle robotic arms. Created written reports presented to the NASA community. -Performed real-time robotics support to on-orbit repairs of broken Solar Array Wing during STS-120 (Flight 10A) -Lead MAGIK Flight analyst for STS-127 (Flight 2J/A). My Analysis and recommendation led to a physical change in the ICC-VLD payload, contributing to mission success.

-Ran physical production and implemented improvements on proprietary materials processing equipment designed to create nano-particulate materials. -Designed and implemented a focused light mechanism to detect hazardous byproducts of material production