Skip to main content

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
Competence Domain:
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:

Executive Summary
PDF

In-orbit manufacturing of very long booms