The EGSE and CCV for ESA VEGA launcher

Abstract

The present paper is aimed at describing the main functionalities and the peculiar architectural aspects of the two systems developed by Vitrociset to support the VEGA launcher Programme in both launcher integration & validation and ground operations. The EGSE (Electrical Ground Support Equipment) is used during the assembly and integration of the stages at ELV premises while the CCV (Centre de Contrôle VEGA) is used on the VEGA launch pad during Launch Vehicle (LV) final integration and count down at the CSG (Centre Spatial Guyanais). The paper briefly outlines and compares the VEGA EGSE and CCV major characteristics and architectural choices, highlighting their innovative and peculiar design, the differences and commonalities.