ÖVE/ÖNORM EN 16603-10-03

This standard addresses the requirements for performing verification by testing of space segment elements and space segment equipment on ground prior to launch. The document is applicable for tests performed on qualification models, flight models (tested at acceptance level) and protoflight models. The standard provides: - Requirements for test programme and test management, - Requirements for retesting, - Requirements for redundancy testing, - Requirements for environmental tests, - General requirements for functional and performance tests, - Requirements for qualification, acceptance, and protoflight testing including qualification, acceptance, and proto-fight models’ test margins and duration, - Requirements for test factors, test condition, test input tolerances, and measurement uncertainties, - General requirements for development tests pertinent to the start of the qualification test programme, - Content of the necessary documentation for testing activities (e.g. DRD). Due to the specific aspects of the following types of test, this Standard does not address: - Space system testing (i.e. testing above space segment element), in particular the system validation test, - In-orbit testing, - Testing of space segment subsystems, subsystems are assumed to be covered in the relevant discipline standards. - Testing of hardware below space segment equipment levels (including assembly, parts, and components), - Testing of stand-alone software,