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Propulsion Engineer


Job Location:

Leander, TX - USA

Monthly Salary: Not provided by the employer
Posted: 30 September 2026 (17 hours ago)
Application Deadline: 28 December 2026
Vacancies: 1 Vacancy

Job Summary

Propulsion Engineer

Location: Leander TX
Work Arrangement: Onsite
Employment Type: Full-Time

Position Overview

We are seeking a Propulsion Engineer to support the development of advanced propulsion and flight vehicle systems. This role combines propulsion design aerodynamics modeling simulation and hands-on testing.

The ideal candidate can translate mission-level requirements into practical engineering solutions and move confidently between first-principles calculations simplified models CFD simulations and physical testing.

Key Responsibilities
  • Translate mission and performance requirements into propulsion and aerodynamic design parameters.
  • Perform rapid engineering analysis using hand calculations analytical models simulation tools and CFD.
  • Design and evaluate solid rocket motors nozzle geometries propellant grain geometries ignition systems and related components.
  • Model internal ballistics pressure dynamics burn-rate behavior and pressure coupling in solid-propellant systems.
  • Optimize propellant grain and core geometries to achieve target thrust profiles and burn characteristics.
  • Analyze thermal and structural loads associated with propulsion systems.
  • Evaluate external aerodynamics across subsonic transonic and supersonic flight regimes.
  • Calculate and validate drag components aerodynamic coefficients flight stability and center-of-pressure versus center-of-gravity relationships.
  • Develop and run CFD simulations to validate assumptions and improve designs.
  • Write code to automate engineering analysis simulation workflows and performance modeling.
  • Work closely with manufacturing systems engineering and testing teams to translate designs into functional hardware.
  • Support ground and flight testing diagnose performance issues and rapidly incorporate findings into design improvements.
Required Qualifications
  • Bachelors degree with 35 years of relevant engineering experience or
  • Masters degree or PhD with 12 years of relevant experience.
  • Strong mechanical engineering fundamentals.
  • Strong understanding of compressible flow gas dynamics thermodynamics and heat transfer.
  • Experience with CFD modeling; ANSYS Fluent is preferred.
  • Proficiency in Python MATLAB or another engineering analysis language.
  • Experience with CAD software such as SolidWorks Onshape or an equivalent platform.
  • Ability to perform accurate first-order engineering calculations.
  • Experience translating performance requirements into engineering design constraints.
  • Ability to work independently and collaboratively in a fast-paced evolving environment.
Propulsion Experience

Experience in several of the following areas is preferred:

  • Internal ballistics and solid-propellant behavior
  • Burn-rate dynamics and pressure coupling
  • Solid rocket motor design
  • Nozzle geometry and performance
  • Propellant grain and core geometry optimization
  • Ignition systems
  • Insulation and high-temperature materials
  • Pressure vessel design and analysis
  • Structural and thermal analysis
  • High-temperature gas flow
  • Solid-propellant formulation
Aerodynamics Experience

Experience in several of the following areas is preferred:

  • External aerodynamics of flight vehicles
  • Missile or projectile design
  • Flight mechanics and trajectory modeling
  • Aerodynamic coefficient modeling
  • Center-of-pressure and center-of-gravity relationships
  • Subsonic through supersonic flow regimes
  • Drag component analysis
  • Flight envelope and stability analysis
  • Guidance navigation and control systems
Ideal Candidate

The successful candidate:

  • Is comfortable solving complex physics problems from first principles.
  • Can move between hand calculations simplified models and high-fidelity simulations while maintaining strong engineering intuition.
  • Makes timely decisions supported by sound technical analysis.
  • Can move projects forward without waiting for perfect information.
  • Enjoys solving difficult and unconventional engineering problems.
  • Is hands-on and willing to work across propulsion aerodynamics manufacturing testing and system integration.
  • Is motivated by designing building and testing real hardware.
  • Demonstrates intellectual curiosity adaptability accountability and a strong bias for action.
Export-Control Requirements

To comply with U.S. government export-control regulations applicants must be a U.S. citizen or national a U.S. lawful permanent resident a qualifying refugee or asylee or otherwise eligible to obtain the required government authorization.