• Preparing test procedure and sequences based on test specifications for spacecraft system testing;

• Planning and leading of AIT operations, including spacecraft Assembly and Integration activities in a cleanroom environment;

• Ensuring all test data is properly collected, catalogued, reviewed, and documented;

• Ensuring testing such as vibration, mass properties measurement, Thermal Vacuum test, alignment and etc. is in compliance with the test requirements document;

• Supporting spacecraft systems functional and performance checks during environmental test;

• Supporting troubleshooting to resolve operations/test anomalies and providing system level building of interfaces for ground equipment and satellite units;

• Overseeing the execution of subsystem and system-level test results, write test reports, document all non-conformances and test anomalies;

• Supporting engineering meetings to collaboratively address identified issues and contribute to finding solutions.

• Minimum of bachelor’s degree in relevant engineering (mechanical engineering is preferable) or science discipline;

• Strong foundation in mathematics and physics.

• Experience in mechanical engineering subject areas for the analysis and test of structures and mechanisms, including engineering mechanics (statics and dynamics), strength of materials, mechanical systems etc.;

• Understanding of stress analysis of structures and mechanical elements is preferable;

• Understanding of thermal analysis is preferable; 

• Good practical knowledge of 3D modelling tools;

• Ability to communicate effectively in English both verbally and written (technical writing, presentation skills) – B2/Upper intermediate;

• Ability to work in team as well as independently;

• Proficiency with MS office (Word, Excel, PowerPoint, Visio);

• Ability to make decisions based on evidence;

• Knowledge about aerospace systems is preferable.