Propulsion Engineer (Vehicle) Verified today
About the Role
Ursa Major is seeking a Propulsion Engineer I (propulsion systems) to support the technical definition, integration, and execution of propulsion systems for hypersonic vehicles. You will serve as a central member of the team, taking immediate ownership of your system as a responsible engineer. This role spans propulsion design, vehicle integration, systems engineering, and test, with ownership from early concept through flight demonstration and production transition.
Key Responsibilities
- Clean sheet design and analysis of fluid and mechanical vehicle components including tanks, structures, feed systems, propellant management, and fluid systems
- Leverage first-principles engineering to drive design and technical decisions
- Support rapid development cycles of new designs and changing requirements including testing, data analysis and hands-on hardware work
- Design modifications of existing components and prototypes to increase performance, improve manufacturability or resolve limitations
- Support test planning and execution, including ground and flight test support
- Participate in failure investigations, nonconformance resolution, and continuous design improvement
- Assembly and testing of first article prototypes
- Collaborate with manufacturing, analysis, and test teams to reduce part-to-part variation and discrepancies
- Work with other engineers on design of components, system sizing, component testing, and system-level architecture
- Interface with customers and external partners during design reviews, technical interchange meetings (TIMs), and integrated product team (IPT) meetings
- Support manufacturing through design for manufacturability (DFM) and producibility considerations
Required Qualifications
- Bachelor's degree in Aerospace Engineering, Mechanical Engineering, or related field
- 1-3 years of experience in propulsion systems engineering or propulsion-focused vehicle development. Strong internship or project/academic club experience in related field acceptable.
- Demonstrated proficiency with computer aided design and drafting
- Knowledge of geometric dimensioning and tolerancing per ASME Y14.5
- Working knowledge of and hands-on experience with fluid, mechanical, and electrical systems
- Desire to take ownership and help wherever needed on the team
- Ability to work in a fast-paced environment and stay flexible based on customer demands and company priorities
- Excellent problem solving, task management, and communication skills
- Ability to obtain and maintain a U.S. Security Clearance
- Must be a U.S. Person (U.S. Citizen or Permanent Resident)
Preferred Qualifications
- Master's degree in Aerospace Engineering or related field
- 1+ years of Siemens NX CAD and Windchill PLM software
- Experience leading design reviews to communicate design decisions and trades
- Experience in design and analysis of tanks, structures or fluids
- Coordination with analysis and lead engineers to quickly mature designs
- Demonstrated proficiency with basic principles of design for manufacturing
- Ability to make sound technical decisions under schedule and performance pressure
- Experience operating in ISO 9001 or AS9100 certified organizations
- Strong understanding of industry standards and requirements
- Demonstrated proficiency with fundamental manual or CNC machining equipment and processes (milling, turning)
- Experience with fluids, structural and thermal analysis using Ansys software
- Liquid propellant rocket engine design, test, or analysis
Compensation and Employment
Full-time Exempt. Base compensation range: $80,000 to $100,000, determined by education, experience, knowledge, skills, and abilities.
Benefits
- Unlimited PTO (vacation, sick, personal, bereavement)
- Paid Parental and Adoptive Leave
- Medical, Dental and Vision Insurance
- Tax Advantage Accounts (HSA/FSA)
- Employer Paid Short and Long Term Disability, Basic Life, AD&D
- Voluntary Life and Emergency Medical Transport options
- EAP Program
- 401k Retirement Savings Plan with Company Match
