include but are not limited to Develop and/or maintain project plans to deliver turbomachinery hardware and sub assemblies in support of development, qualification and flight hardware test Develop, manage and report progress on the team's scope, schedule, cost, and resource & hardware plans Manage, prioritize, and report progress of engineering release, assembly, acceptanc

include but are not limited to Perform and lead engineering activities including Fault Tree Analysis (FTA), Functional Hazard Assessments (FHAs), Hazard Reports, Failure Modes Effects and Criticality Analyses (FMECA), reliability analysis, and developing mitigation plans Develop plans and coordinate completion of system and subsystem safety analysis, providing review, guid

include but are not limited to Responsible for leading the Component level Thermal Analysis team or the System level Thermal Analysis team within the Thermal Analysis group. Perform personnel management including performance reviews, time cards, training, etc. Recruit, hire, manage, and mentor a diverse, equitable, and inclusive team. Manage your direct reports' profession

include but are not limited to Architect and develop Unpressurized and Pressurized Docking System test plans and procedures. Provide technical leadership to the team, advising on test approaches, and bringing your experience to bear on our most challenging technical problems in docking systems. Mentor & train other team members. Develop and lead complete life cycle of the

include but are not limited to Thermal analysis of rocket engine turbomachinery and valves at varying levels of maturity and detail Meticulous bookkeeping of model status and changes over time Defining and anchoring thermal predictions of turbomachinery and valve components and assemblies to test data Advocating for methods that will improve component and analysis performa

include but are not limited to Serve as a thermal systems integrator, working and negotiating across the multiple integrated product teams (IPTs) between the CDE and its supporting spacecraft. Develop interface control documents (ICDs) and support the development of interface requirements documents (IRDs) that may pertain to a subsystem focus. Drive system and subsystem le

Design mechanisms for space flight which may include, engine gimbaling mechanisms, docking systems, solar and radiator deployment systems, hatches, and deployable or retractable external covers. Participate in the entire design cycle of flight hardware, including conceptual and detailed design, trade studies, structural analysis, development testing, and qualification.Gen

include but are not limited to Own and lead the Ventilation and Atmosphere Revitalization fan assemblies and interfaces through the entire life cycle Conception, Design, Build, Test, Install and Operations Derive functional and performance requirements, and specify hardware Perform system calculations and basic analyses Design and integrate the fan assemblies and acoustics

include but are not limited to Design and optimize cleaning methods for a variety of materials, including metals, plastics, and composites to meet precision cleanliness levels. Evaluate and select appropriate cleaning materials, chemicals, and equipment to achieve desired surface finishes. Collaborate with product design and manufacturing teams to integrate cleaning and su

include but are not limited to Evaluate and select metallic materials for usage in liquid rocket engines, taking into consideration mechanical properties, thermal properties, and environmental factors. Collaborate with design and manufacturing teams to integrate material and process requirements into the overall vehicle or system design. Ensure specialized processes used i

include but are not limited to Coordinate with relevant design teams to optimize the inspection of hardware including GTAW weldments, laser welded hardware, additive manufactured components, and castings Build manufacturing and in service NDT procedures and methods Must be willing to inspect production hardware for acceptance as required Design reference standards for comp

At Blue Origin, we envision millions of people living and working in space for the benefit of Earth. We're working to develop reusable, safe, and low cost space vehicles and systems within a culture of safety, collaboration, and inclusion. Join our diverse team of problem solvers as we add new chapters to the history of spaceflight! As the Manager of a diverse and hardwor

Evaluate and select nonmetallic materials and coatings for thermal protection and other applications, taking into consideration thermal properties, mechanical properties, and environmental factors. Collaborate with design and manufacturing teams to integrate TPS requirements into the overall vehicle or system design. Act as M&P signatory for engineering drawings for rocke

include but are not limited to Coordinate with relevant design teams to optimize the inspection of hardware including GTAW weldments, laser welded hardware, additive manufactured components, and castings Build manufacturing and in service NDT procedures and methods Must be willing to inspect production hardware for acceptance as required Design reference standards for comp

include but are not limited to Facilitate and perform system safety and reliability analyses, identify hazards, failure causes and mitigations, and provide a detailed record of the safety risk approach Confirm maintainability engineers are engaged in ensuring design for maintainability is considered in the development process Balance operational efficiency and engine opera