■Key Responsibilities
・Collaborate with other sub-system teams of Structure, Thermal, GNC, Avionics, Operation and AIT, supporting the lander propulsion design to a consistent system for current and future mission.
・Support the propulsion team with technical point of view. Validate analysis and model in the propulsion team, provide hands-on feedback and modification plan, and intervene those technical tasks as showing a better alternative approach if necessary. Prepare the related technical reports, obtaining the approvals from the stakeholders.
・Support propulsion design efforts for spacecraft system development with proposing practical applications such as trade-off studies, material, component, and manufacturing process selection while watching the feasibility in the project.
・Find technical conflicts beyond the sub-system level and lead a solution through sub-system and system level discussions.
・Support the creation and/or the maintenance of the spacecraft propulsion system relevant documents such as -sub-system requirement specification and sub-system design specification.
・Support FMECA, launcher requirement, and the range safety related to the propulsion system.
・Support the completion of the design reviews with closing the action items.
・Support manufacturing, procurement, hardware assembly, integration, testing, and launch operation related to the propulsion system, which may include travel to the sites sometimes.
・Evaluate component level and EPM tests related to the propulsion subsystem. Coordinate with suppliers if necessary.
・Prepare operational plan and input to other sub-system teams of Avionics, Thermal, GNC, and Mission.
・Report status and issues to the team lead and the group manager.
・Support to build a strong team with effective communications in the team.
・Maintain proactive coordination between the teams to balance and achieve project goal.