DIN EN 16602-60-05:2014-12

The objective of this standard is to define the requirements for the procurement of hybrid microcircuits for use in space systems. This standard covers the following requirement domains: validation procedure for a hybrid microcircuit manufacturer; design of hybrid microcircuits; procurement of active and passive chips; procurement of materials and piece parts; screening of hybrid microcircuit lots; lot acceptance tests for hybrid microcircuits; customer involvement, key inspection points; repair provisions; hybrids and data package delivery. The procurement requirements for hermetic hybrid microcircuits for use in space projects are defined in this standard. This standard also provides details concerning the documentation requirements and the procedures relevant to obtain approval for the use of hybrid microcircuits in the fabrication of space systems and associated equipment. The provisions of this standard apply to all participants in the production of space systems, at all levels and are applicable to manned and unmanned spacecraft, launchers, satellites, payloads, experiments, and their corresponding organizations. This standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S-ST-00. This document (EN 16603-70-32:2014) has been prepared by Technical Committee CEN/CLC/TC 5 "Space", the secretariat of which is held by DIN (Germany). This document has been developed to specifically cover space systems and therefore has precedence over any European Standard since it covers the same scope but with a wider domain of applicability (for example aerospace). The responsible German body is Working Committee NA 131-10-01 AA "Interoperabilität von Informations-, Kommunikations- und Navigationssystemen" ("Interoperability of information, communication and navigation systems") of the DIN Standards Committee Aerospace (NL).