Job Description On the Miranda propulsion engineering team, we are responsible for designing, developing, and testing the Miranda first stage engine. We are directly responsible for developing an engine that meets vehicle performance and quality requirements on a tight schedule. In this role, you will work across the full lifecycle of hardware, including requirements definition, design, analysis, development, test, and qualification of the engine system. The core engine team requires deep technical knowledge, extreme ownership, and clear communication with our cross-functional teams. The successful candidate will have a strong interest in flight hardware ownership, will be extremely adaptable to new challenges, and has a strong desire to make impactful contributions to the next launch vehicle. This role is primarily responsible for designing and releasing the integrated engine system including complete fluids systems and secondary structures interfacing with engine and vehicle hardware. RESPONSIBILITIES Responsible for producing and releasing Miranda fluids system designs interfacing with integrated combustion devices, turbomachinery, valves, fluid systems, TVC, and avionics components. Own and execute development, qualification, and acceptance testing of engine systems and sub-systems. Responsible for close coordination with other engineers, production team members, and Quality department to produce and release numerous engine sub-assembly and component drawings that maximize performance and reduce manufacturing complexity. Maintain multiple, controlled revisions of the engine CAD as component designs are traded in analysis and iterated in development testing. Provide hands-on support for development engine builds to iterate and improve engine design and layout. Develop and maintain engine interfaces. Participate in test stand and vehicle installation procedures and improve them as needed. Communicate risks and trade solutions to minimize risk of failure in development, manufacturing, test and flight. We are a company committed to creating diverse and inclusive environments where people can bring their full, authentic selves to work every day. We are an equal opportunity/affirmative action employer that believes everyone matters. Qualified candidates will receive consideration for employment regardless of their race, color, ethnicity, religion, sex (including pregnancy), sexual orientation, gender identity and expression, marital status, national origin, ancestry, genetic factors, age, disability, protected veteran status, military or uniformed service member status, or any other status or characteristic protected by applicable laws, regulations, and ordinances. If you need assistance and/or a reasonable accommodation due to a disability during the application or recruiting process, please send a request to HR@insightglobal.com.To learn more about how we collect, keep, and process your private information, please review Insight Global's Workforce Privacy Policy: https://insightglobal.com/workforce-privacy-policy/. Skills and Requirements Bachelor’s Degree in Mechanical Engineering, Aerospace Engineering, or equivalent. 3+ years experience with CAD and configuration management tools (Siemens NX and Teamcenter preferred). Experience working within large CAD assemblies. Familiarity with GD&T fundamentals, applications, and tolerance stackups. Strong background in mechanical design and metallic manufacturing techniques including subtractive and additive machining, welding, and inspection. Understanding of bipropellant liquid rocket fundamentals and ability to collaborate with subject matter experts to maximize engine performance. Knowledge of material selection for cryogenic, high pressure, and high temperature systems as well as Oxygen-compatible materials. Knowledge of fluid components such as valves, regulators, pressure transducers, tubing, pressurized hardware, seals, and instrumentation and experience performing fluid systems sizing analysis with such components. History of developing solutions with partially defined requirements and changing criteria. Advanced degree in Mechanical Engineering, Aerospace Engineering, or equivalent field Experience with liquid rocket or in-space propulsion engines or systems. Experience in aerospace flight production programs. Knowledge of multi-disciplinary CAD modules and interfaces (pipe routing, electrical routing, sheet metal, etc.). Experience and interest in automating virtual workflows and tools. Experience reducing the complexity of large integrated assemblies to reduce part count, cost, and lead time. Full hardware lifecycle ownership – from blank sheet design to full operation.