The double insulation topic has become a very important issue in the satellite design since its implementation drives the sizing of the whole satellite electrical architecture. Different approaches and solutions have been proposed by Industry [2], according to specific need of each spacecraft design and requirements. According to ECSS-E-ST-20C [1]., a barrier against short circuit between conductors or circuit elements shall be guaranteed also after any credible single failure. In particular., the guideline is that all non-protected elements of a main bus distribution system shall implement an electrical double insulation up to the first protection device (e.g.: fuse., current breaker or current limiter).


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    Title :

    Implementation of double insulation at satellite level: an approach




    Publication date :

    2019-09-01


    Size :

    2929828 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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