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Functional Testing of a Hold-Down-Mechanism under Thermal-Vacuum Conditions
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Functional Testing of a Hold-Down-Mechanism under Thermal-Vacuum Conditions
Testaufbau Force-Margin-Test CAD
Testvorbereitung für den Niederhaltemechanismus
Testaufbau in der TV-Kammer
Performance of functional tests for a Hold-Down-Mechanism in thermal vacuum conditions
Evaluation of the avaiable force margin
Design and realization of a special test setup to determine the force margin
Project details
Core competencies:
Space
Customers:
AIRBUS Defence & Space
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