Specter Aerospace
Propulsion Test Engineering Co-Op - Spring 2027
Peabody, Massachusetts
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- Seniority
- Mid level
- Country
- US
- Work mode
- On-site / unstated
- First seen by hirly
- 2 Sept 2026
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the posting
Role Summary
Specter Aerospace is seeking a Propulsion Test Engineer Co-op (4-6+ month cycle) to be a significant contributor to the development and testing of hypersonic propulsion systems. Those in this role will have the opportunity to take ownership in the design, manufacturing, and test of advanced ramjet/scramjet engine hardware. A successful candidate will have a passion for both hands-on work and the analysis of thermofluid systems.
Note: Specter hires both Propulsion Design Engineer Co-ops and Propulsion Test Engineer Co-ops from this application, depending on an applicant’s interest and experience. Please submit an application to this posting if you are interested in either position.
About Specter Aerospace
Specter Aerospace is building the next generation of hypersonic vehicles for U.S. Forces and Allies. With offices in Boston and Peabody, MA, Specter leverages its advanced propulsion technologies, manufacturing, and testing capabilities to rapidly develop supersonic and hypersonic systems. Our Propulsion Test Engineering will be based in our Peabody office. Funded by a mix of government R&D organizations and private funding, Specter is expanding its team in preparation for flight testing and full-scale production.
- Specter offers a wide diversity of tasks, projects, and technical exposure, all while providing co-ops with the same resources and project ownership as our full-time staff members. Our co-ops work closely with experienced engineers and scientists to complete projects that are critical to the mission of the company.
- Role Responsibilities
Take ownership in propulsion subsystem/component development from ideation to first-article test and characterization
Design and manufacture engine components, test stand hardware, and piping/tubing systems leveraging in-house machining capabilities
Conduct engine and propulsion component testing in a direct-connect hypersonic testing facility
Develop thermofluids and propulsion performance an alysis code (Python/MATLAB)
Participate in design reviews and technical discussions across multidisciplinary vehicle sub-system groups
Required Qualifications
Pursuing a bachelor’s degree in mechanical engineering, aerospace engineering, or equivalent
Experience with CAD software (SolidWorks preferred)
Prior hands-on experience in a technical shop, lab, or student organization
Comfort with project autonomy, fast-paced work environments, and design ownership
Fundamental understanding of core mechanical engineering principles, especially those relating to thermofluids (Fluid mechanics, heat transfer, gas dynamics)
Eligible to obtain and maintain a U.S. Secret security clearance (U.S. Citizenship required )
Ability to pass a pre-employment drug screen and background check
Preferred Qualifications
Previous professional OR student team (FSAE, SEDS, AIAA, etc . ) project experience relevant to the requirements for this position
Previous experience in positions that involve fluid dynamics, thermodynamics, gas dynamics and/or combustion
MATLAB or Python experience , especially in the development of thermofluids analysis tools
Hardware design and build experience in rocket engine s or ram/scramjet engine platforms
Experience in the manufacture and troubleshooting of fluid systems consisting of valves, pumps, tubing, piping, etc.
Ability to diagnose and troubleshoot issues relating to data acquisition systems (LabView, PLCs) and test stand sensors (pressure transducers, thermocouples, load cells)
Experience with creating plumbing and instrumentation diagrams (P&IDs)
Previous experience with manual machining, CAM, design for manufacture, and design for additive manufacture
EEO Statement
All qualified applicants will receive consideration for employment without regard to race, color, religion, sex, sexual orientation, gender identity, national origin, disability, or veteran status.
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