Propulsion Systems Design Engineer

General Qualifications

• Graduated from Mechanical, Aeronautical, Automotive, or Aerospace Engineering departments of universities,
• Preferably holding a master’s degree in one of these disciplines,
• Proficient in engineering fields such as statics, dynamics, strength of materials, thermodynamics, heat transfer, and fluid mechanics,
• Knowledgeable in at least one CAD modeling software (preferably Catia),
• Capable of designing systems and subsystems based on requirements,
• Knowledgeable in geometric dimensioning and tolerancing,
• Skilled in the use of applied engineering tools and systems,
• Familiar with literature review processes and capable of conducting comprehensive literature research,
• Strong problem-solving skills,
• Proficient in technical English,
• Good command of MS Office applications,
• Open to innovation and self-development oriented,
• Possessing strong communication skills and able to work well in a team environment,
• Able to adapt to a high-paced work schedule and flexible working hours,
• Preferably experienced in unmanned aerial vehicle (UAV) propulsion systems,
• Capable of working in coordination with other teams related to areas of responsibility.

Job Description

Assignments will be made considering the project dynamics and the requirements of active division of labor, including;

• Defining subsystem requirements for engine integration into the aerial vehicle (cooling system, exhaust, engine mounts, air inlets, etc.),
• Designing parts required for subsystems and engine integration,
• Designing the engine exhaust system with attention to thermal variables and participating in testing activities,
• Identifying propellers and related subsystems, and conducting design work for integration,
• Performing lifespan calculations for products,
• Preparing and publishing technical documentation related to propulsion systems,
• Ensuring verification of system products through testing, analysis, and simulation methods.