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

Finite Element Model development, refinement, validation, and correlation to tests Rigid and flexible body dynamics Modeling, simulation, and verification of spacecraft launch, docking, and landing events Acceleration, shock, and vibration measurement and data interpretation of ground and flight tests General loads development for spacecraft and related ground systems Sup

Finite Element Model development, refinement, validation, and correlation to tests Rigid and flexible body dynamics Modeling, simulation, and verification of spacecraft launch, docking, and landing events Acceleration, shock, and vibration measurement and data interpretation of ground and flight tests General loads development for spacecraft and related ground systems Sup

Finite Element Model development, refinement, validation, and correlation to tests Rigid and flexible body dynamics Modeling, simulation, and verification of spacecraft launch, docking, and landing events Acceleration, shock, and vibration measurement and data interpretation of ground and flight tests General loads development for spacecraft and related ground systems Sup

Develop & manage Thermal specifications and requirements (at subsystem and component levels) Develop & manage Thermal interfaces, including Interface Control Documents (ICDs) and models (in collaboration with adjacent IPTs) Decompose requirements from system and subsystem levels into lower level requirements Mentor early career Thermal Systems Engineers on the Lunar Progr

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 position is part of the Space Syst

include but are not limited to Design, simulate, and optimize thermal management systems for ISRU technologies, with a focus on high temperature and high current applications, including reactors and electrolysis systems. Participate in all product development stages, from conceptualization through design, to implementation, integration, and environmental testing in space a

include but are not limited to Responsible for directing a technical team to design mass efficient vehicle structures and reliable mechanisms that satisfy requirements, and comply with intra vehicle interfaces. Recruit, hire, manage, delegate to, and mentor a diverse, equitable, and inclusive team Manage your direct reports' professional development (e.g., hiring, performa

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 Support early feasibility studies, subsystem architecture development, definition of subsystem and component trade space, and concept of operations for the Fuel Cell Controller's Avionics Hardware and Software Derive and develop subsystem requirements, perform analyses and trades to validate requirements, and maintain subsystem specification,

Design of various pressure vessel types, and shapes to accommodate vehicle space allocation and integration envelope. Design of fluid lines and flex elements for cryogenic and space application. Drawing generation, including tolerance and GD&T setup. Ownership of design release cycle, including drawings release, and DFM reviews. Analysis of primary and secondary spacecraf

Design of various pressure vessel types, and shapes to accommodate vehicle space allocation and integration envelope. Design of fluid lines and flex elements for cryogenic and space application. Drawing generation, including tolerance and GD&T setup. Ownership of design release cycle, including drawings release, and DFM reviews. Analysis of primary and secondary spacecraf

include but are not limited to Drives the development of thermal systems, including system architecture definition, thermal system modeling, component sizing, and design. Perform trade studies relating to the selection of material and subsystem hardware. Perform hand calculations to screen concepts without detailed modeling and to sanity check finite element model results.

include but are not limited to Develop System Level Finite Element Models (FEM) based on interaction with the design and engine system analysis team. Use structural analysis methods to support test and failure investigations Derive shock & vibration levels for Engine components based on test data Support component qualification and acceptance testing Instrumentation select

include but are not limited to Perform structural analysis in support of engineering nonconformances and anomalies during engine production, test, and fleet service. Support production driven continuous improvement initiatives such as cost and producibility design changes. Develop production structural analysis methodology and process improvements to streamline post develo