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Launch System Electrical Avionics Engineer
2018-05-04 15:26:30| Space-careers.com Jobs RSS
The work covers the following technical domains Launch System AIT definition and control of measurement plans in test requirements and execution, definition of technical specifications for the procurement of specific ground measurement acquisition and storage equipment. Electrical interfaces schematics integration and analysis, electrical performances analyses e.g. power supply transient and steadystate analyses, measurement accuracy, others. System EMC verifications groundingbonding quality measurement, CECS, RERS. Realtime systems modelling, analysis, specification and troubleshooting. Computers for realtime onboard applications, both as selfcontained units and as embedded items in subsystem equipment. The work includes system design for faulttolerant computer systems, component design and development, operating systems, and identification of tools and methods for dependable specification, design and testing. Data systems for onboard data communication, spacecraft system operation under ground control and with onboard autonomy, groundonboard data communication, and for manned spaceflight crew informatics and interfaces. This includes data system standards and specific software, e.g. data communication software. Data storage, i.e. onboard solidstate mass memory systems, including architecture, components, interfaces, packaging technologies, and operational usage. Electronic design essentially for the implementation of digital functions related to onboard data systems. Payload data acquisition and processing chains, including digital and image processing techniques and devices. Specific tasks A diverse range of support tasks is required to be carried out within the above tasks, encompassing hardware, software and system aspects in support to the Ariane 6 project. These can be grouped within the following main headings Definition of technical specifications for the procurement of HWSW items. Evaluation of verification analyses and reports. Participation in reviews and meetings. Overseeing the Launch System Combined Tests and Launch Campaign qualification tasks. Requeriments Knowledge of electrical systems architectures of a launch system. Knowledge of TTE protocol and its implementation. Knowledge of main serial data exchange protocols and endtoend wired measurement chains. Understanding of main Launch System RF communications. Experience in equipment procurement, subsystems integration and testing. Experience in spacecraft project support in particular related to spacecraft data handling. Knowledge of the space environment, related standards and space quality requirements.
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electrical
launch
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Category:Transportation and Logistics