Structural Analysis for a Satellite Propulsion Modul

 Home / Projects / Space / Structural Analysis for a Satellite Propulsion Modul
Propulsion module for a satellite (CAD)
Propulsion module for a satellite (CAD)

FE model of the satellite propulsion module
FE model of the satellite propulsion module

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)

Project details

Core competencies: Space
Customers: ArianeGroup

KRP Mechatec GmbH is an engineering services provider specialized in structural tests and analyses in the field of space, aviation, experimental research and other high-tech industries, certified according to DIN EN ISO 9001:2015.

 
KRP Mechatec GmbH
Boltzmannstr. 2
85748 Garching
 
Telefon
Telefax
E-Mail
Internet
+49 (0)160 9482 1904
+49 (0)8131 505 331
info@krp-m.de

Certifikate ISO 9001:2015