Johns Hopkins Applied Physics Lab

Aerospace Propulsion Engineer

Johns Hopkins Applied Physics Lab$100K — $245K *
Aerospace & Defense
5 - 7 years of experience
Job Overview by Ladders

Qualifications

  • Bachelor's degree in Aerospace Engineering, Mechanical Engineering, Physics, or related field.
  • 5+ years of relevant experience or equivalent demonstrated expertise.
  • Direct experience in designing or analyzing scramjet and dual-mode ramjet propulsion systems.
  • Extensive background in applying CFD to compressible reacting flows with finite-rate chemistry.
  • Knowledge of integrated inlet, isolator, combustor, and nozzle performance.

Responsibilities

  • Lead design and analysis of scramjet and dual-mode ramjet components.
  • Apply high-fidelity CFD techniques to complex reacting-flow problems.
  • Investigate combustion phenomena and propulsion dynamics.
  • Plan verification and validation studies for computational models.
  • Compare computational results with empirical test data.
  • Diagnose and recommend modifications based on simulation outcomes.
  • Enhance workflows related to computational and high-performance computing.
  • Communicate technical findings effectively to various stakeholders.

Benefits

  • Access to cutting-edge technology and projects in hypersonic propulsion.
  • Opportunities for mentorship and technical leadership development.
  • Participation in national defense projects directly impacting aerospace innovation.
  • Collaborative work environment with industry partners and government sponsors.
Full Job Description
Description

Are you excited to help shape the future of hypersonic propulsion and solve some of the nation's most challenging aerospace engineering problems? Do you want to tackle hypersonic propulsion challenges where the answers aren't already known?

If so, we're looking for someone like you to join our team at APL.

We are seeking a Senior Aerospace Propulsion Engineer with expertise in scramjet or dual-mode ramjet design and high-fidelity modeling. You will support critical U.S. Department of Defense programs by designing, analyzing, and troubleshooting advanced hypersonic air-breathing propulsion systems.

The successful candidate will recognize the governing physics, frame ambiguous technical problems, select and defend appropriate analysis methods, and turn incomplete or conflicting evidence into actionable recommendations.

As an APL Senior Aerospace Propulsion Engineer, you will...
  • Lead the design and analysis of integrated scramjet inlet, isolator, combustor, and nozzle flowpaths.
  • Apply high-fidelity CFD with finite-rate chemistry to compressible reacting-flow problems.
  • Investigate phenomena such as shock trains, unstart, fuel-air mixing, ignition, flameholding, combustion stability, thermal choking, and propulsion-airframe interaction.
  • Plan and assess verification, validation, mesh-sensitivity, and model-sensitivity studies.
  • Compare computational predictions with ground-test, flight-test, and lower-order analysis results.
  • Diagnose unexpected test or simulation behavior and recommend design, analysis, or test changes.
  • Improve computational, meshing, post-processing, and high-performance-computing workflows.
  • Communicate conclusions to Government sponsors, industry partners, and technical teams.
  • Provide technical leadership and mentorship to other engineers.

Qualifications

You meet our minimum qualifications for the job if you...
  • Possess a bachelor's degree in Aerospace Engineering, Mechanical Engineering, Physics, or a related field.
  • Have five or more years of relevant experience, or equivalent expertise demonstrated through advanced research and technical accomplishments.
  • Have direct experience designing or analyzing scramjet, dual-mode ramjet, or related high-speed propulsion flowpaths.
  • Have substantial experience applying CFD to compressible reacting flows using finite-rate chemistry.
  • Understand integrated inlet, isolator, combustor, and nozzle performance and operability.
  • Have experience evaluating mesh quality, numerical convergence, modeling assumptions, and simulation credibility.
  • Can independently frame unfamiliar technical problems, challenge assumptions, and develop defensible recommendations.
  • Have experience with Linux and technical programming or scripting using Python, MATLAB, C++, Fortran, or similar languages.
  • Possess strong written and oral communication skills.
  • Are able to obtain a Secret level security clearance. If selected, you will be subject to a government security clearance investigation and must meet the requirements for access to classified information. Eligibility requirements include U.S. citizenship.

You'll go above and beyond our minimum requirements if you...
  • Possess an advanced degree in hypersonic propulsion, combustion, compressible flow, or computational fluid dynamics.
  • Have led an integrated scramjet or dual-mode ramjet design or analysis effort.
  • Have experience with scale-resolving reacting-flow simulations such as LES or hybrid RANS/LES.
  • Have correlated CFD with direct-connect, free-jet, wind-tunnel, or flight-test data.
  • Have experience with uncertainty quantification, design optimization, solver development, MPI, or GPU computing.
  • Have experience with relevant tools such as CFD++, US3D, VULCAN-CFD, GridPro, Pointwise, Tecplot, Cantera, or equivalent tools.
  • Have an active Secret clearance.

Minimum Rate

$100,000 Annually

Maximum Rate

$245,000 Annually

About Johns Hopkins Applied Physics Lab

The Johns Hopkins University Applied Physics Laboratory (APL) is a research and development organization that provides solutions to national security and scientific challenges. The laboratory was founded in 1942 and is located in Laurel, Maryland. APL is a division of the Johns Hopkins University and is a not-for-profit organization. The laboratory has expertise in a variety of areas, including space exploration, national security, and healthcare.
Learn more about Johns Hopkins Applied Physics Lab
Size
7,000 employees
Industry
Founded
1942

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