In-orbit manufacturing of very long booms
Programme Reference
G617-083MS
Status
Closed
Country
United Kingdom
Start Date
2015
End Date
2017
Programme: GSTP Prime Contractor: MAGNA PARVA LTD
Objectives
To develop a technology allowing the in-orbit manufacturing of very long, slender composite booms for large aperture applications.
Description
Techniques to in-orbit manufacture very long booms (from 20m up to approximately 50m and more) have been addressed in the past by looking at in- orbit bonding of thin-walled composite booms. Composite technology also allows the direct manufacturing of a long, continuous, constant cross section beam by means of a pultrusion process, permitting the achievement of lengths, up to 200m, with potential superior accuracy/stability performances. The present activity aims at a re-engineering the pultrusion process in order to make it applicable to in-orbit manufacturing of very long booms. Low power consumption heating system will be a key feature of the re-engineered pultrusion machine. The activity would include the realization of a prototype (BB) pultrusion machine to be operated in vacuum, to demonstrate the feasibility of the in-orbit boom production. Short length booms (100-300mm) will be produced and mechanically tested.
• Application domain: Generic Technologies
•
Technology Domain:
15 - Mechanisms
15 - Mechanisms
•
Competence Domain:
2-Structures, Mechanisms, Materials, Thermal
2-Structures, Mechanisms, Materials, Thermal
• Initial TRL: TRL 4
• Target TRL: TRL 5
• Achieved TRL: TRL 3
•HarmoRoadMap: Deployable Booms & Inflatable Structures (2010.2)
•IPC Document: ESA/IPC(2014)61,add.1
•Public Document: