The future of aerospace and defense starts here. Ursa Major was founded to revolutionize how America and its allies access and apply high-performance propulsion, from hypersonics to solid rocket motors, satellite maneuvering and launch. We design and deliver propulsion and defense systems that solve the most urgent and critical national security demands. As a Propulsion Analysis Engineer II, you will primarily focus on structural analysis of vehicles and propulsion systems.  You will be exposed to multiple vehicles, systems, and engines, along with the unique challenges each present. We are looking for analysts who bring new skills and best practices from their prior experience to Ursa and who, in time, will mentor others. You will be expected to support verification and validation efforts and to provide proactive feedback to our design team based on the results of your work. Lastly, as Ursa ramps up its production rate and begins development on new engine platforms, you will be expected to assess nonconforming hardware, introduce approaches that could improve our team’s efficiency, and venture into additional analysis specialties to support others in our multi-disciplinary analysis team. You will report to our Propulsion Analysis Team Lead. This role is available to work remotely within the US (with 10% travel to Colorado) or as a hybrid or on-site role out of our Berthoud, Colorado office. Responsibilities: You will evaluate our designs through static, dynamic, fatigue, and fracture analyses and provide recommendations when needed to achieve our objectives. You will support GFEM development for vehicles and propulsion systems You will propagate loads to vehicle and engine components You will perform coupled thermal-stress analysis to assess material response under extreme conditions You will verify and validate your models You will work closely with our test team to request the instrumentation necessary to anchor our analytical models You will perform loads development for vehicles and engine programs You will collaborate with other engineering teams to develop our systems while ensuring they meet requirements and comply with the structural standards we follow Minimum Experience/Requirements: B.S. degree in mechanical, aerospace engineering, or a comparable field 2+ years of professional experience performing structural analysis Experience performing Finite Element Analysis (FEA / FEM) using commercial codes (e.g., ANSYS, Abaqus, or NASTRAN-based solvers) High Cycle Fatigue Analysis (HCF, crack initiation predicted by a stress-life / SN approach) A strong theoretical background in structural mechanics Comfortable working in a fast-paced, startup environment Ideal Experience/Requirements: M.S. degree or higher in Mechanical, Aerospace Engineering, or a comparable field, ideally focusing on solid mechanics, fatigue, fracture, or structural dynamics Thermal-Structural static analysis (particularly dealing with nonlinear materials and large strains) GFEM development and model grounding experience Dynamic analysis methods (modal, random vibration, shock response) Working experience in loads development Low Cycle Fatigue Analysis (LCF, crack initiation predicted by a strain-life / e-N approach) Fracture analysis (crack growth / safe-life and assessing for instability via LEFM, ideally with prior experience using NASGRO) A strong theoretical background in heat transfer, fluid mechanics, and/or compressible flow Experience with the ANSYS FEA suite Experience with Femap/Nastran Experience anchoring analytical models to physical testing Knowledge of turbomachinery-related analytical methods (e.g., generating Campbell diagrams to assess margins on rotordynamics or structural modes or rotating hardware) Prior professional experience working on either rocketry or turbomachinery Experience supporting failure investigations and root-cause analysis A track record of working efficiently in fast-paced engineering environments A track record of effective oral and written communications to support your recommendations Fluid analysis (e.g. Computational Fluid Dynamics / CFD or 1-D transient analysis using SINDA/FLUINT or ROCETS) Knowledge of composite materials, insulation, and ablative thermal protection systems Colorado law requires us to tell you the base compensation range of this role, which is $95,000 - $115,000, determined by your education, experience, knowledge, skills, and abilities. What we can’t quantify for you are the exciting challenges, supportive team, and amazing culture we enjoy. Click here for more information about our awesome benefits. Classification: Full-time Exempt Benefits Include: (Please note, Interns are not eligible for benefits) Unlimited PTO - Vacation, Sick, Personal, and 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 Additional Benefit Options Including Voluntary Life and Emergency Medical Transport EAP Program Retirement Savings Plan - 401k with Company Match Equity Grants in the Company How To Apply: Interested candidates are encouraged to apply by filling out the application below and clicking "Submit Application". This position will be posted for a minimum of 3 days and will remain open until filled or adjusted based on the volume of applicants. NOTE: Research suggests that women and BIPOC individuals may self-select out of opportunities if they don't meet 100% of the job requirements. We encourage anyone who believes they have the skills and the drive necessary to succeed here to apply for this role. US CITIZENSHIP, PERMANENT RESIDENCY, REFUGEE OR ASYLUM STATUS IS REQUIRED. Eligibility to obtain and maintain a U.S. Security Clearance. We’re an equal-opportunity employer. You will be considered for employment without attention to race, color, religion, sex, sexual orientation, gender identity, national origin, veteran, or disability status. No outside recruiters, please.