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:\u2022 Requirements for test programme and test management,\u2022 Requirements for retesting,\u2022 Requirements for redundancy testing,\u2022 Requirements for environmental tests,\u2022 General requirements for functional and performance tests,NOTE Specific requirements for functional and performance tests are not part of this standard since they are defined in the specific project documentation.\u2022 Requirements for qualification, acceptance, and protoflight testing including qualification, acceptance, and protofight models' test margins and duration,\u2022 Requirements for test factors, test condition, test tolerances, and test accuracies,\u2022 General requirements for development tests pertinent to the start of the qualification test programme,NOTE Development tests are specific and are addressed in various engineering discipline standards.\u2022 Content of the necessary documentation for testing activities (e. g. DRD).Due to the specific aspects of the follow ing types of test, this Standard does not address:\u2022 Space system testing (i.e. testing above space segment element), in particular the system validation test,\u2022 In-orbit testing,\u2022 Testing of space segment subsystems,NOTE Tests of space segment subsystems are often limited to functional tests that, in some case, are run on dedicated models. If relevant, qualification tests for space segment subsystems are assumed to be covered in the relevant discipline standards.Testing of hardware below space segment equipment levels (including assembly, parts, and components),\u2022 Testing of stand-alone software, NOTE For verification of flight or ground softw are, EN 16603-40 (ECSS-E-ST-40) and EN 16602-80 (ECSS-Q-ST-80) apply.\u2022 Qualification testing of tw o-phase heat transport equipment,NOTE For qualification testing of tw o-phase heat transport equipment, EN 16603-31-02 (ECSS-E-ST-31-02) applies.\u2022 Tests of launcher segment, subsystem and equipment, and launch facilities,\u2022 Tests of facilities and ground support equipment,\u2022 Tests of ground segment.This activity will be the update of EN16603-10-03:2014NOTE: Parallel development of update of EN Standard and the new European TR17603-10-03.<\/p>\n","protected":false},"excerpt":{"rendered":"
Space engineering – Testing (Draft)<\/b><\/p>\n\n\n
\n Published By<\/td>\n Publication Date<\/td>\n Number of Pages<\/td>\n<\/tr>\n \n DIN<\/b><\/a><\/td>\n 2021-07<\/td>\n 139<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n","protected":false},"featured_media":532819,"template":"","meta":{"rank_math_lock_modified_date":false,"ep_exclude_from_search":false},"product_cat":[832,2635],"product_tag":[],"class_list":{"0":"post-532807","1":"product","2":"type-product","3":"status-publish","4":"has-post-thumbnail","6":"product_cat-49-140","7":"product_cat-din","9":"first","10":"instock","11":"sold-individually","12":"shipping-taxable","13":"purchasable","14":"product-type-simple"},"_links":{"self":[{"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/product\/532807","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/product"}],"about":[{"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/types\/product"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/media\/532819"}],"wp:attachment":[{"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/media?parent=532807"}],"wp:term":[{"taxonomy":"product_cat","embeddable":true,"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/product_cat?post=532807"},{"taxonomy":"product_tag","embeddable":true,"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/product_tag?post=532807"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}