CONTRACT (Rolling) OR PERMANENT
Rate Negotiable
Electronics Engineer x1
• Assessment of power demands from the effector electronic systems, throughout the flight to determine the required battery size and management
• EMC testing of NKE payload with mock up of effector electronic assembly
• Initial discussions with potential suppliers on available solutions - to inform performance values input to modelling.
• Establish power requirements across the flight profile, based on component power demands and when different components are active across the flight. Query if we need two independent batteries for critical systems (FTS/S&A)
• Design of Ground based INS solution to be integrated with one-way effector internal IMU and GNSS solution