{"id":532885,"date":"2024-11-05T16:04:00","date_gmt":"2024-11-05T16:04:00","guid":{"rendered":"https:\/\/pdfstandards.shop\/product\/uncategorized\/din-en-16603-50-14\/"},"modified":"2024-11-05T16:04:00","modified_gmt":"2024-11-05T16:04:00","slug":"din-en-16603-50-14","status":"publish","type":"product","link":"https:\/\/pdfstandards.shop\/product\/publishers\/din\/din-en-16603-50-14\/","title":{"rendered":"DIN EN 16603-50-14"},"content":{"rendered":"<p>This standard specifies a common set of spacecraft onboard electrical interfaces for sensor acquisition and actuator control. The interfaces specified in this standard are the traditional point-to-point interfaces that are commonly used on modern spacecraft.The interfaces specified in this standard include analogue and discrete digital interfaces used for status measurement and control, as wellas point-to-point serial digital interfaces used for digital data acquisition and commanding of devices.This standard specifies:? interface signal identification;? interface signal waveforms;? signal timing requirements;? signal modulation;? voltage levels;? input and output impedance;? overvoltage protection requirements;? bit ordering in digital data words;? cabling requirements where appropriate.This standard does not cover:? connector requirements;? digital data word semantics;? message or block formats and semantics.Connector requirements are not covered because these are normally mission or project specific. The goal of this standard is to establish a single set of definitions for these interfaces and to promote generic implementations that can be re-used throughout different missions. When referred, the present standard is applicable as a complement of the already existing interface standards ANSI\/TIA\/EIA-422B-1994and ITU-T Recommendation V.11 (Previously ?CCITT Recommendation?) ? (03\/93).Guidance for tailoring of the present standard can be found in Annex A.This Standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS S ST-00.<\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Space engineering &#8211; Spacecraft discrete interfaces<\/b><\/p>\n<table style=\"width: 100%\" border=\"0\" cellspacing=\"0\" cellpadding=\"0\">\n<tbody>\n<tr>\n<td>Published By<\/td>\n<td>Publication Date<\/td>\n<td>Number of Pages<\/td>\n<\/tr>\n<tr>\n<td><a href=\"https:\/\/pdfstandards.shop\/product-category\/publishers\/din\/\"><b>DIN<\/b><\/a><\/td>\n<td>2014-12<\/td>\n<td>77<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n","protected":false},"featured_media":532900,"template":"","meta":{"rank_math_lock_modified_date":false,"ep_exclude_from_search":false},"product_cat":[832,2635],"product_tag":[],"class_list":{"0":"post-532885","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\/532885","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\/532900"}],"wp:attachment":[{"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/media?parent=532885"}],"wp:term":[{"taxonomy":"product_cat","embeddable":true,"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/product_cat?post=532885"},{"taxonomy":"product_tag","embeddable":true,"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/product_tag?post=532885"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}