Spaceflight Propulsion Engineer

RESPONSIBILITIES:

• Apply fluid mechanics, thermodynamics, heat transfer, materials, structures, and machine-design principles to propulsion and spacecraft pressure systems.
• Independently perform or lead propulsion and pressure-system analyses.
• Develop, review, and validate fluid-flow, pressure-system, thermodynamic, and thermal models.
• Develop and maintain engineering analysis and data-processing tools using Python, MATLAB, or similar software.
• Evaluate system architectures and lead or contribute to technical trade studies.
• Establish technical assumptions, document analysis methods, and communicate results and limitations.
• Assess component-to-system and system-to-vehicle technical effects.
• Provide technical oversight of propulsion components, suppliers, and hardware-development activities.
• Review designs, drawings, material selections, fabrication methods, assembly processes, and acceptance criteria.
• Support or lead propulsion hardware development from concept through fabrication, assembly, test, integration, and operation.
• Plan, coordinate, witness, or evaluate component- and system-level tests.
• Review acceptance-test data, qualification reports, verification evidence, and flight-readiness documentation.
• Evaluate test results and determine whether the available evidence satisfies technical and program requirements.
• Lead or support investigations of anomalies, nonconformances, and unexpected system behavior.
• Develop technically defensible recommendations for issue disposition and risk mitigation.
• Review and coordinate closure of variances, nonconformance reports, hazard reports, changes, waivers, reuse documentation, and certification action items.
• Develop verification approaches and support formal certification of propulsion systems and flight hardware.
• Assess pressure-system safety, cleanliness, contamination-control, and hardware-integration requirements.
• Support propulsion-system integration with spacecraft, test vehicles, or small satellites.
• Coordinate technical activities with NASA program and project offices, spacecraft organizations, suppliers, prime contractors, sub-tier contractors, and international partners.
• Organize and track concurrent document reviews, technical issues, risks, and action items.
• Delegate or coordinate reviews with appropriate hardware and technical points of contact.
• Prepare and present technical status, risks, nonconformances, and recommendations to program stakeholders.
• Participate in mission simulations, vehicle checkouts, propulsion console operations, and flight support.
• Provide technical guidance and mentoring to less experienced engineers.
• Travel to supplier, test, integration, launch, or program locations when required.
• Other duties as required.

REQUIRED:

This position has been posted at multiple levels (must meet minimum level indicated). Depending on the candidate's experience, requirements, and business needs, we reserve the right to consider candidates at any level for which this position has been advertised.

• This position requires US Citizenship or Permanent Resident status due to the sensitivity of customer related information.
• This position requires experience in the space industry or Department of Defense/Department of War.
• Must have a bachelor's degree in engineering.
• Must have a minimum of 5 years of recent and related work experience.
• Demonstrated knowledge of fluid mechanics and thermodynamics.
• Working knowledge of heat transfer, engineering materials, mechanical systems, structures, or machine design.
• Experience analyzing propulsion, pressure, fluid, or thermal systems.
• Experience supporting hardware development, testing, integration, certification, or operation.
• Experience processing, analyzing, and interpreting engineering or test data.
• Ability to evaluate requirements, technical drawings, analyses, test plans, test results, and verification evidence.
• Ability to investigate technical issues and develop defensible engineering recommendations.
• Ability to assess component-level issues in a broader system and vehicle context.