Propulsion Staff Engineer – Thruster Systems - (APSE080626.1)

Cimarron•Houston, TX

6d•Onsite

About The Position

Cimarron is seeking an experienced Propulsion Staff Engineer – Thruster Systems to own the end-to-end technical execution of a bipropellant thruster from requirements definition through design, build, integration, test, and flight readiness. You will lead cross-functional teams and suppliers to deliver to aggressive cost and schedule targets while maintaining safety and configuration discipline. The ideal candidate combines deep hands-on propulsion hardware experience with strong technical leadership, clear communication, and a bias for execution. This is an onsite position located in Houston, TX.

Requirements

Due to facility security requirements, only U.S. citizens or permanent residents are eligible for consideration at this time.
Ability to complete a pre-employment background check and drug screening, which will include but is not limited to testing for marijuana use.
Must be willing to work evenings and weekends as needed to meet critical project milestones.
10 or more years of relevant experience in spacecraft or launch vehicle propulsion, with demonstrated depth in thruster or liquid rocket engine design and development.
Significant hands-on experience with engine/thruster design, development, qualification, and integration — including injectors, combustion chambers, nozzles, igniters, and thermal management interfaces.
Expertise in combustion, thermodynamics, heat transfer, and fluid dynamics with demonstrated application to thruster performance and thermal analysis.
Experience developing and executing test campaigns including test planning, instrumentation selection, and data correlation.
Propulsion component experience spanning valves, filters, regulators, manifolds, and instrumentation interfacing with thruster assemblies.
3D modeling software experience: SolidWorks preferred.
Bachelor’s degree from an accredited college or university in Aerospace, Mechanical, or related Engineering discipline required; advanced degree preferred

Nice To Haves

SolidWorks preferred

Responsibilities

Own the end-to-end technical execution of bipropellant thruster assemblies including combustion chambers, injectors, nozzles, igniters, and associated valves/instrumentation – from requirements through, design, build, integration, test and flight readiness.
Serve as a subject matter expert in thruster design, providing technical authority on system architecture, sizing, fluid/thermal/structural analyses, materials/manufacturability, and performance optimization across the full development lifecycle.
Perform detailed modeling, analysis and simulation of thruster assemblies using tools such as ANSYS, Fluent, TDK, CEA, etc to evaluate combustion performance, thermal effects, structural margins and transient behaviors.
Perform component sizing and selection for thruster assemblies, ensuring compatibility with performance, thermal, structural, safety and compatibility requirements.
Design, plan and execute thruster development, qualification, and acceptance test campaigns define instrumentation requirements, execute test planning and perform data correlation to anchor and validate analytical models.
Lead and participate in internal and external design and gate reviews, trade studies, and subassembly integration activities; ensure compliance with system requirements and program milestones.
Coordinate and manage technical requirements and design verification activities with external vendors and suppliers, interface on cost, schedule, design, manufacturing, and acceptance.
Lead and participate in trade studies, component selection, and subassembly design and integration analyses in support of thruster development programs.
Provide technical mentorship and guidance to less experienced engineers.
Responsible for delivering against performance, safety, cost, and schedule targets.