Design of space hardware using a CDF like methodology (AMCDF)
Programme Reference
15/007
Status
Closed
Country
Germany
Start Date
2018
End Date
2019
Programme: Discovery Prime Contractor: OHB System AG
Description
The project aimed to establish a structured approach to an optimised part or component by applying Concurrent Design methods. It intended to incorporate all necessary disciplines and competencies that are required for a potential spacecraft part. Within the activity, advanced manufacturing included various novel techniques, not only additive manufacturing. It means that the Concurrent Design approach was developed for the engineering of units to be built with a broad range of advanced manufacturing technologies.
• Application domain: Generic Technologies
•
Technology Domain:
24 - Materials and Manufacturing Processes
08 - System Design & Verification
24 - Materials and Manufacturing Processes
08 - System Design & Verification
•
Competence Domain:
02 - Structures / Mechanisms / Materials / Thermal
02 - Structures / Mechanisms / Materials / Thermal
• Initial TRL: TRL N/A
• Target TRL: TRL N/A
• Achieved TRL: TRL N/A
•Public Document: