Satellite Avionics Design Engineer
GENERAL QUALIFICATIONS
• Graduated from university departments such as Electronics Engineering, Electrical and Electronics Engineering, Electronics and Communication Engineering, Aerospace Engineering, Mechatronics Engineering, or related fields,
• Believing in the importance of developing nationally and indigenously critical technologies for our country in the space sector,
• Experienced in analog and digital circuit/system design,
• Experienced in control methods for power distribution systems,
• Has developed projects using circuit design and simulation tools,
• Preferably experienced in microcontroller-based circuit development projects,
• Preferably knowledgeable and experienced in communication interfaces such as RS232/422/485, CAN Bus, SPI, UART, I2C, Ethernet, SpaceWire, and PCIe,
• Experienced in using laboratory equipment such as oscilloscopes, power supplies, load banks, signal generators, etc.,
• Preferably experienced in developing electronic hardware compliant with space or military standards such as ECSS-S-ST-E-20, MIL-STD-461, MIL-STD-704, MIL-STD-810,
• Preferably knowledgeable about electromagnetic interference/electromagnetic compatibility (EMI/EMC),
• Possesses a good level of technical English for research and documentation,
• Analytical thinker, open to development, eager to learn, and strong in problem-solving,
• Willing to demonstrate perseverance, dedication, and commitment to ensure the success of ongoing projects,
• Able to adapt to flexible working hours in a fast-paced work environment,
• No travel restrictions,
• Eager to be part of a young and dynamic R&D team that is motivated to work with team spirit in the space domain where engineering is applied at the highest level.
JOB DESCRIPTION
• Designing and testing avionics hardware used in spacecraft,
• Establishing the hardware design architecture and writing lower-level system requirements,
• Designing hardware and managing the testing, manufacturing, and integration processes of the designed hardware,
• Determining the electrical power requirements of aircraft platforms according to different test configurations, and performing capability and adequacy analyses of the power architecture,
• Performing hardware simulations, executing test processes, and analyzing and reporting the results,
• Supporting improvements to hardware designs by conducting analyses and tests to address issues encountered during testing processes and in the space environment,
• Ensuring effective coordination with software, mechanical, manufacturing, integration, and system management teams,
• Contributing to the creation of the most optimal design by reviewing reports from other design disciplines and evaluating their requirements.