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

2. 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 more than sufficient
No contamination sensitive areas
FGS storage temp.: -100 °C °C
FGE storage temp.: -50 °C °C
Mechanical constraints
No special mechanical treatment necessary
FGS delivered in Aluminium sealed containers

3. 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