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! This role is part of the Lunar Permanen

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! We are a diverse team of collaborators,

include but are not limited to Perform structural analysis of rocket engine turbomachinery in support of engineering nonconformances and anomalies during production, test, and fleet service. Conduct detailed structural analysis using FEA and classical methodology on turbomachinery components such as impellers, turbines, and housings. Conduct fatigue and fracture calculatio

include but are not limited to Responsible for leading and coordinating engineering operations activities for Lunar Product Engineering in support of the MK1 and MK2 landers and National Team partners for common hardware. Develop a set of simple but consistent processes for management and reporting of products status, escalations, issues, and resolutions. Assist the MK1 an

Participate as technical evaluation committee chair for Thermal design reviews of lunar landers and other spacecraft programs at Blue Origin Represent the company and project with key customers and partners Provide peer review to thermal design and analysis products Provide technical recommendations to multiple established spacecraft thermal design and analysis teams Prov

include but are not limited to Design and maintain CAD models of mechanical and mechatronics components and systems, including tools, fixtures, jigs, structures, and focusing on rapid prototyping and production using Creo & Windchill. Generate detailed drawings from CAD models and incorporate annotations for geometric dimensioning and tolerancing (GD&T) as per ASME Y14.5.

include but are not limited to Lead the development, documentation, and updating of test procedures, including Standard Operating Procedures (SOPs), Job Hazard Analyses (JHAs), and detailed test plans to ensure operational excellence and compliance with safety standards. Own the setup, operation, and maintenance of environmental test systems, primarily vacuum chambers, for

include but are not limited to Ownership of one or more Mission Crew Interfaces components or subassemblies throughout the entire product lifecycle. Support subsystem Responsible Engineers by providing component and subassembly trade studies, analyses, performance characterization and specification, detail design, device selection, roadmap direction, test planning and exec

Design and develop vehicle autonomous system management and fault management flight software Support design and development of flight software functional architecture for orbital space system Design and develop embedded computer vision software for autonomous proximity operations and docking Evaluate, decompose, and create requirements for safety critical, real time opera

Develop subsystem management and Displays & Control application flight software Work with cross functional stakeholders to define software concepts of operations, functions and requirements Author unit tests, documentation, and participate in design and code reviews Integrate Displays & Control applications with vehicle management applications Develop and run unit tests,

include but are not limited to Support early concept studies, architecture development, definition of GN&C mode states and transitions, and concept of operations. Derive and develop GN&C requirements, perform analyses and trades to validate requirements, and maintain subsystem specification, and performance metrics . Collaborate with other subsystem and spacecraft systems

include but are not limited to Baseline implementation plans for technical standards with Blue Origin and NASA technical leads and manage the work with element SE&I leads through the verification process. Establish the process for requirement variances (deviations, waivers, and exceptions) and manage the production, review, and closeout of all variances against Program and

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! We are a diverse team of collaborators,

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 Design and code automated test equipment software to support formal and informal verification of avionics requirements (qualification and acceptance testing) Develop and maintain user interface for running verification tests on the engine controllers Establish and follow software development processes to ensure test equipment software is reli