FGM S/C Integration Requirements

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FGM S/C Integration Requirements Werner Magnes Institut für Weltraumforschung (IWF) Austrian Academy of Sciences

Constraints Safety and dependability constraints Normal precaution No pyros, batteries, radioactive material, pressurized containers etc. No limited life time items Environmental constraints Clean room class 100.000 more than sufficient No contamination sensitive areas FGS storage temp.: -100 °C ... +100 °C FGE storage temp.: -50 °C ... +65 °C Mechanical constraints No special mechanical treatment necessary FGS delivered in Aluminium sealed containers

Electrical constraints Constraints / MLI Electrical constraints Connector savers will be used for sensor and FGE connector No restrictions to power ON/OFF during on-ground testing Inputs to system level tests Mu-metal can for all flight sensors (MGSE) All functional tests before and after environmental tests Test MLI blankets (supplied by UCB, TBC) Vibration TV / TB EMC (TBC) FGS MLI Test MLI replaced by Flight MLI at launch site