NICOLINI, GianalfredoGianalfredoNICOLINI2024-06-252024-06-252017http://hdl.handle.net/20.500.12386/35241The present document collects the contribution given by the whole Metis Team.The EID-B defines the PI response to the technical requirements in part A, specifying in detail the interface information applicable to Metis. Furthermore, in this document, the Metis requirements versus the S/C are univocally identified and numbered. Part B will form the sole formal and binding document for all technical and programmatic agreements between the ESA Solar Orbiter Project Office and the Principal Investigator. The EID A and B will be placed under formal configuration and change control once signed and thus any change requires formal agreement between ESA and the PI. The EID- B will become one of the applicable documents to the Solar Orbiter prime contractor. Since the EID-B will accompany Metis until its realization, we have chosen to introduce the description of the interfaces with the S/C and some sections have been added to describe l the optical characteristics and the performance of the instrument.ELETTRONICOenResearch reportING-IND/05 - IMPIANTI E SISTEMI AEROSPAZIALIERC sectors::Physical Sciences and Engineering::PE8 Products and Processes Engineering: Product design, process design and control, construction methods, civil engineering, energy systems, material engineering::PE8_1 Aerospace engineering