Aerospace Engineer
CurrentCurrently, I am assigned to the Space Nuclear Propulsion (SNP) project, responsible for development of the Model Based Systems Engineering (MBSE) models and methods. Previously, I was in the Mission & Fault Management group for the Human Landing System (HLS) and Space Launch System (SLS), working on Functional Fault Analysis, Abort Effectiveness Analysis, Safing False Positive Analysis, and Detailed Verification Objectives. An SLS or HLS Abort is when the crew has to maneuver the vehicle during flight to avoid an explosion or other malfunction, so it is a safety-critical event. The Aborts area is a very complex, interdisciplinary task involving engineers from the areas of avionics and software design, structural failures, safety & mission assurance, and from across program elements. During this assignment I helped define the abort conditions, identify abort triggers, and analyze how effective they will be in a given launch vehicle failure scenario.Previously I was the Change Package Engineer responsible for the SLS Core Stage to Core Stage Engine Interface Control Document (ICD). In this position, I learned the technical details of the RS-25 Core Stage Engine (Space Shuttle Main Engine) and how it operates to propel the SLS. In addition to the Core Stage engine, I worked in the same role on the Exploration Upper Stage to Exploration Upper Stage Engine ICD, which will use a smaller engine than the RS-25. Prior to the ICD assignment I was the lead for the SLS Functional Analysis. The effort was concerned with analyzing the functional behavior, interfaces, and requirements of the launch vehicle, spacecraft, and ground systems that NASA is designing to take future astronauts Beyond Earth Orbit (BEO). I was working with Systems Modeling Language (SysML) in the Enterprise Architect tool, which is a relatively new approach at NASA.