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Temporary Propulsion Test Engineer Jobs in Ohio (NOW HIRING)

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Temporary Propulsion Test Engineer information

What is a temporary propulsion test engineer?

A Temporary Propulsion Test Engineer is a specialized engineer hired for a limited period to conduct and oversee tests on propulsion systems, such as rocket engines or jet engines, in aerospace or automotive industries. Their responsibilities include preparing test setups, analyzing data, ensuring safety protocols, and reporting results to help validate or improve engine designs. These roles are often project-based and may require experience with specific testing equipment and software. Temporary positions allow companies to scale their workforce for critical testing phases without long-term commitments.

What is the difference between Temporary Propulsion Test Engineer vs Propulsion Systems Engineer?

AspectTemporary Propulsion Test EngineerPropulsion Systems Engineer
CredentialsEngineering degree, testing certificationsEngineering degree, systems design certifications
Work EnvironmentTest facilities, labs, outdoor test sitesDesign offices, integration labs, testing facilities
Industry UsagePrimarily in testing and validation phasesDesign, development, and integration of propulsion systems

The Temporary Propulsion Test Engineer focuses on conducting tests and validating propulsion components, often in test facilities. In contrast, the Propulsion Systems Engineer is involved in designing and developing propulsion systems throughout the product lifecycle. Both roles require engineering credentials and are integral to aerospace and defense industries, but their daily tasks and focus areas differ significantly.

What are the key skills and qualifications needed to thrive as a temporary propulsion test engineer?

To thrive as a Temporary Propulsion Test Engineer, you need a solid background in mechanical or aerospace engineering, experience with propulsion systems, and often a relevant engineering degree. Familiarity with test instrumentation, data acquisition systems, and safety protocols—as well as certifications like FE or EIT—are typically required. Strong problem-solving skills, attention to detail, and effective communication help you excel in dynamic test environments. These competencies ensure accurate test execution, reliable data collection, and safety compliance, which are critical for propulsion system development.

What types of projects and teams can a temporary propulsion test engineer expect to work with during their assignment?

As a Temporary Propulsion Test Engineer, you will often be assigned to specific propulsion system projects, such as rocket engine development or aircraft engine testing. You'll typically work closely with multidisciplinary teams that include design engineers, technicians, and safety specialists to plan and execute test campaigns. Your daily responsibilities may involve preparing test setups, monitoring test data in real time, troubleshooting issues, and ensuring all procedures comply with safety standards. The fast-paced, project-based nature of this role offers valuable exposure to cutting-edge technology and can help you build relationships and experience that may lead to longer-term opportunities in the industry.
What are the most commonly searched types of Propulsion Test Engineer jobs in Ohio? The most popular types of Propulsion Test Engineer jobs in Ohio are:
What job categories do people searching Temporary Propulsion Test Engineer jobs in Ohio look for? The top searched job categories for Temporary Propulsion Test Engineer jobs in Ohio are:
What cities in Ohio are hiring for Temporary Propulsion Test Engineer jobs? Cities in Ohio with the most Temporary Propulsion Test Engineer job openings:

Research Aerospace Engineer

The University of Dayton

Dayton, OH • On-site

Full-time

Medical, Dental, Vision, Retirement, PTO

Posted 4 days ago


University Of Dayton rating

8.4

Company rating: 8.4 out of 10

Based on 6 frontline employees who took The Breakroom Quiz

98th of 617 rated colleges and universities


Job description

Research Aerospace Engineer

Apply now Job No: 503787
Work Type: Staff Full Time (1500 hours or greater)
Location: Dayton, OH
Category: Research Institute Staff
Department: Air Vehicle Optimization - 250571
Pay Grade: R1/R2 - Exempt
Advertised: August 07, 2026
Applications close: August 21, 2026

Position Summary:

UDRI is seeking qualified applicants to apply for a Research Aerospace Engineer position. This position will work for the Air Vehicle Optimization Group of the Structures & Materials Division and is a full-time benefit eligible position that offers health, dental and vision insurance, retirement, disability, tuition assistance, vacation/sick accrual and holiday pay.

The Air Vehicle Optimization Group at UDRI is a diverse team of skilled engineers and scientists who work closely with the Air Force Research Laboratory (AFRL) to develop, prototype, and test numerical models, software, and hardware for the multidisciplinary design and analysis of aerospace vehicles. The group brings together specialties in Aerospace, Electrical, and Mechanical Engineering, Computer Science, Mathematics, and Physics to combine state-of-the-art engineering tools with innovative ideas to support future aircraft design methods from conceptual design through flight testing. A few of the projects the group currently supports include: Computational Aircraft Prototype Synthesis (CAPS), Missile Enhancement via Reconfigurable Interceptor Nose, Efficient Supersonic Aircraft Vehicle, X-56, XQ-58, Effectiveness Assessment of Concepts and Technologies, and Sensitivity Analysis for Multidisciplinary Systems.

The group is currently seeing an Aerospace Engineer to support ongoing research and development contracts at Wright-Patterson Air Force Base in the Air Force Research Laboratory to provide support for airframe propulsion and power systems integration. Research Aerospace Engineers apply fundamental engineering principles to design, develop, document, maintain, and deploy software infrastructure and engineering analyses in the support of aerospace engineering research. Specifically providing support in the area of conceptual vehicle design in support of our Modular/Scalable UAS portfolio and perform finite-element-based structural sizing processes.

The successful candidate will bring to bear their skills and experience with one or more of the following: experience in aircraft design and propulsion and power system integration, finite element analysis for structural analysis, CFD for aerospace analysis, multidisciplinary analysis, sensitivity analysis, design optimization, aeroservoelastic design optimization, and aircraft trajectory optimization framework, and computer programming. Strong communication and interpersonal skills are essential and highly valued in this role.

Minimum Qualifications:

- A Bachelors or equivalent degree in Aerospace Engineering, Mechanical Engineering or related discipline from ABET accredited institution
- Knowledge of: propulsion systems, aeroelasticity, experimental aerodynamics, numerical analysis, CFD, orbital dynamics
- Basic experience with MATLAB, LabVIEW, Python, SolidWorks, OpenVSP, XFOIL, Cradle CFD, C++/Ansys or other similar programming languages
- Experience with developing 3D printed parts
- Due to requirements of our research contracts with the U.S. federal government, candidates for this position must be a US Citizen

R1 Level Requirements:
Bachelors and no previous work experience
R2 Level Requirements:
Bachelors and three years previous work experience, OR
Masters and two years previous work experience

Preferred Qualifications:

While not everyone may possess all of the preferred qualifications, the ideal candidate will bring many of the following:

- A Masters or equivalent degree in Mechanical Engineering, Aerospace Engineering, or related discipline from ABET accredited institution
- Proficient using MATLAB, LabVIEW, Python, SolidWorks, OpenVSP, XFOIL, Cradle CFD, C++/Ansys or similar programming languages
- Experience in designing and executing test procedures for parametric studies
- Experience with analyzing experimental data and presenting results
- Experience with mechanical design, experimental testing and validation, fluid mechanics, structural analysis, additive manufacturing, systems integration
- Experience with CFD tools
- Experience with designing and modifying propulsion test hardware
- Research experience

Special Instructions to Applicants:

To apply please submit a cover letter addressing each minimum qualification and any applicable preferred qualifications that you meet.

Closing Statement:

Informed by its Catholic and Marianist mission, the University is committed to the dignity of every human being. Informed by this commitment, we seek to increase diversity in all of its forms, achieve fair outcomes, and model inclusion across our campus community. The University is committed to policies of affirmative action designed to increase the employment opportunities of individuals with disabilities and protected veterans in compliance with the Rehabilitation Act of 1973 and Vietnam Era Veterans' Readjustment Assistance Act of 1973.

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