These tasks shall be performed for in-house and out-of-house design and development projects.
#Bastion technologies about verification#
Perform and/or assess hazard analyses to assure that: (a) all hazards are identified and the associated risks properly characterized (b) hazard controls satisfy applicable safety requirements and adequately mitigate safety risks (c) safety verification requirements are clearly identified and adequate, including the clear definition of verification pass/fail criteria and (d) the safety verification status is properly maintained in a closed loop accounting system.Ensure safety engineering support for program/project hardware/design milestone reviews through all phases of development (from concept through manufacturing to final acceptance) to ensure design compliance with safety requirements.Perform system-level safety analysis and developed approaches for risk mitigation.Review component Interface Design Document and Interface Control Documents to ensure completeness of safety analysis.Coordinate with engineering, management and NASA Customer to exchange technical data to support the development of the safety analysis.Prepare and maintain System Safety Analysis Reports (including Hazard Reports) by identifying and evaluating severity and probability of vehicle system hazards and cross-program hazards.Review and prepare engineering and system safety analysis, technical reports, engineering change proposals, verification data, and other documentation.Provide technical and programmatic oversight of spacecraft subsystems.Ensure new systems (and those that have been repaired) meet requirements mandated by NASA and specifications set by manufacturers.Be knowledgeable of safety processes to include Inspection/Verification. Conduct research to address problems associated with flight safety systems.Apply system safety analysis techniques in the design of safety-critical products. Assist Vehicle Integration Team with the design/development of SLS compliance with Safety and Mission Assurance (SMA) requirements.
Candidate shall provide the QD35 Technical Lead/Branch Chief with critical information needed for task team assignments, knowledge where certain disciplines or skill sets reside within the greater team, assurance of evenly distributed work load, and ability to answer questions with regard to team capabilities.Individual may be requested to travel to MAF/KSC for the upcoming vehicle integration in support of the SLS launch. Work with NASA Customer on the assignment and distribution of tasking across the team to include tracking/maintenance of System Safety Team responsibilities and information.
Develop and utilize SMA-specific tools needed to assure that all applicable system safety requirements (e.g., Agency, Center, Program/Project, etc.) are identified for MSFC programs and projects.Core responsibilities include contributing to the design and development of aerospace vehicle systems and processes from a safety perspective, documenting various system safety analyses, and assisting with safety-related requirements management. The Safety Engineer will be responsible for system safety assessments for all Programs and Projects within the QD35 Vehicle System Branch of the Mission Systems Assurance for Marshall Space Flight Center (MSFC) Safety and Mission Assurance (SMA) Directorate.
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