What are the responsibilities and job description for the Test Engineer position at EVONA?
Test Engineer – Vibration & Thermal Vacuum
Role Overview
The Test Engineer is a key technical contributor responsible for leading vibration and thermal vacuum testing activities for spaceflight hardware. This role owns test campaign execution, ensures compliance with program requirements, and serves as a technical authority for environmental verification efforts.
Responsibilities
- Lead the development and execution of vibration and TVAC test campaigns from concept through final reporting.
- Define test strategies, requirements, and acceptance criteria in collaboration with systems and design teams.
- Operate and oversee the use of shakers, thermal vacuum chambers, and instrumentation systems.
- Provide real-time oversight of testing, including anomaly detection, troubleshooting, and decision-making.
- Ensure all testing complies with applicable aerospace standards and customer requirements.
- Direct test setups including fixturing, sensor selection, placement, and calibration.
- Lead failure investigations and root cause analyses for test nonconformances.
- Deliver comprehensive test reports with data analysis, conclusions, and recommendations.
- Maintain readiness of test facilities and support continuous improvement initiatives.
- Mentor junior engineers and technicians as needed.
Required Qualifications
- Bachelor’s degree in Mechanical Engineering, Aerospace Engineering, or related field.
- 3 years of professional experience in aerospace environmental testing.
- Demonstrated expertise in vibration and thermal vacuum testing methodologies.
- Strong understanding of spacecraft environmental requirements and verification processes.
- Experience with data acquisition systems, instrumentation, and test data analysis.
- Proven ability to work cross-functionally and communicate technical results clearly.
Preferred Qualifications
- Experience with test automation or analysis tools such as LabVIEW, MATLAB, Python, or TestStand.
- Background supporting spacecraft or launch vehicle qualification programs.
- Knowledge of MIL-STD-1540, MIL-STD-810, ECSS, or NASA standards.
- Familiarity with thermal or structural modeling and correlation activities.