Skip to main content
Skip to navigation
Skip to footer
DLR Portal
Press
Accessibility
de
en
Institute of
Structures and Design
About us
About us
▾
The Institute of Structures and Design
▾
Departments
▾
Automation and Quality Assurance in Production Technology
▾
Component Design and Manufacturing Technologies
▾
Ceramic Composites and Structures
▾
Structural Integrity
▾
Space System Integration
▾
Locations & Arrival
▾
Stuttgart
▾
Augsburg
Research & Transfer
Research & Transfer
▾
Research Topics
▾
High-Performance Lightweight Structures
▾
CMC Technology and Structures
▾
Lightweight Structures for Space Applications
▾
Aero Engine Structures
▾
Projects
▾
Ongoing projects
▾
Project archive
▾
Research infrastructure
▾
Start-Ups
Latest
Latest
▾
News
▾
Events
▾
Press review
Multimedia
Multimedia
▾
Publications
▾
Videos
Careers & Education
Careers & Education
▾
Job vacancies at the institute
▾
Information for students
>
About us
>
Departments
>
>
Space System Integration
>
REFEX
Home
>
About us
>
Departments
>
Space System Integration
>
REFEX
REFEX
REFEX
For the DLR flight experiment REFEX, the department is responsible for the design and construction of the metallic structure of the missile, the folding wings and the fibre composite fairings.
Credit:
DLR (CC BY-NC-ND 3.0)
