Development of the interstage 2/3 of the new launcher VEGA C to be realized in the frame VECEP program with a composite grid structure.
Design and sizing of the interstage 2/3 of launcher VEGA C with a composite grid structure;
Manufacturing of the Technological Model (TMO) and Demonstrator Model (DMO) using a winding technology patented by CIRA;
Technological transfer and support to Avio for the manufacturing and qualification of the Qualification Model (QMO) and Flight Unit (FU).
Programma VECEP – Assignment of Interstage 2/3 for VEGA C launcher