Structural Analysis for a Satellite Propulsion Modul

Structural Analysis for the qualification of a Satellite Propulsion Module:

• Modal - analysis
• Quasi - static loads
• Sine - vibration loads
• Random - vibration loads
• Verficiation of pressurized tubing system
• Development of required notching for sine- and reandom-vibration tests
• Test prediction
• FE model in Femap/Nastran
• Derivation of reduced models for Coupled Load Analysis (Craig-Bampton-Methode)