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Ursa Major

Develops launch-ready propulsion engines for space

Senior Design Engineer - Solid Rocket Motor Nozzles

PropulsionConfirmed live in the last 24 hours
Full-timeBerthoud, CO, USA

About the Job

Requirements

  • A bachelor's degree in aerospace engineering, mechanical engineering, or a related field is required.
  • At least 5 years of relevant experience in rocket propulsion, high-temperature structures, or closely related hardware is required.
  • Demonstrated experience with erosive and nonerosive nozzle designs and associated manufacturing practices is required.
  • Ability to execute clean-sheet nozzle designs, including first-order fluid and thermal analyses to inform geometry, materials, and insulation strategies, is required.
  • Proficiency with CAD and engineering analysis tools, such as structural, thermal, and fluid or computational fluid dynamics analysis, is required.
  • In-depth knowledge of thermodynamics, fluid dynamics, heat transfer, and structural mechanics is required.
  • Ability to work autonomously within a defined scope and to involve subject matter experts or technical leads when needed is required.
  • Clear written and verbal communication skills for cross-functional collaboration, design reviews, customer discussions, and documentation are required.
  • Eligibility to obtain and maintain a U.S. Department of Defense Secret clearance is required as a condition of employment.
  • The candidate must be a U.S. Person, including a U.S. citizen or permanent resident.

Responsibilities

  • Lead the design of solid rocket motor nozzles, including shells, insulators, and interfaces, with minimal guidance from subject matter experts.
  • Translate customer requirements and mission needs into manufacturable nozzle designs that meet performance, reliability, cost, and schedule targets.
  • Lead design trades across materials, manufacturing processes, and nozzle architectures.
  • Plan and support development test campaigns to reduce risk for new concepts and mature them into qualified products.
  • Review test data and post-test hardware to verify performance against predictions, identify anomalies, and drive design or process changes when needed.
  • Provide hands-on support during builds and tests by integrating hardware, resolving build issues in real time, and connecting design and manufacturing feedback.
  • Drive collaboration with analysis, manufacturing, test, systems, and supply chain teams to ensure nozzle designs meet stakeholder needs.
  • Maintain project schedules, identify key risks early, and work with technical leads to implement mitigation plans.
  • Generate and review CAD models and engineering drawings in accordance with internal standards and ASME Y14.5-2009/2018.
  • Maintain organized technical documentation, including requirements, design reviews, test plans and reports, and verification and validation evidence.
  • Provide day-to-day technical guidance to junior engineers in nozzle design, materials, and manufacturing.

Desired Qualifications

  • A master's degree or PhD in mechanical engineering, aerospace engineering, or a related technical discipline is desired.
  • Experience architecting and designing electromechanical systems, such as actuators and gimbal mechanisms, for nozzle vectoring is desired.
  • Direct experience with vectorable nozzle technologies, such as splitline designs, jet tabs, and flexseals, is desired.
  • Hands-on involvement in rapid product development environments, including prototype-heavy and fast-iteration programs, is desired.
  • Experience designing hardware for high-rate automated production, including design for manufacturing and assembly and process automation, is desired.
  • Proficiency with Siemens NX for CAD and Ansys for finite element and computational fluid dynamics analysis is desired.
  • An active U.S. Department of Defense Secret clearance or higher is desired.

About the Company

Ursa Major

Develops launch-ready propulsion engines for space

Ursa Major Technologies designs, tests, and manufactures propulsion systems for aerospace, focusing on engines for space launch vehicles and hypersonic applications. Its propulsion engines are designed, tested, and then sold or licensed to customers as launch-ready systems that can be integrated into rockets or hypersonic platforms for dependable liftoff. The company differentiates itself by delivering reliable, cost-effective engines that are ready-to-deploy, targeting both commercial and governmental clients to reduce the risk of launch failures. Its goal is to power the future of space exploration and hypersonic travel by providing engines that balance performance, reliability, and cost to help customers overcome financial, technical, and time barriers to propulsion development.

Company size
501-1,000
Company stage
Debt Financing
Total funding
$426.5M
Headquarters
Berthoud, CO
Founded
2015

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