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Normas DIN – AENOR
DIN EN 16603-20-06:2014-09

DIN EN 16603-20-06:2014-09

Space engineering - Spacecraft charging; English version EN 16603-20-06:2014

Ingéniérie spatiale - Charges électrostatique des vehicules spatiales; Version anglaise EN 16603-20-06:2014

Raumfahrttechnik - Aufladung von Raumfahrzeugen; Englische Fassung EN 16603-20-06:2014

Fecha Anulación:
2020-11 /Withdrawn
Equivalencias internacionales:

EN 16603-20-06 (2014-07)

Relación con otras normas DIN:
This standard is a standard within the ECSS hierarchy. It forms part of the electrical and electronic engineering discipline (ECSS-E-ST-20) of the engineering branch of the ECSS system (ECSS-E). It provides clear and consistent provisions to the application of measures to assess, in order to avoid and minimize hazardous effects arising from spacecraft charging and other environmental effects on a spacecraft?s electrical behaviour.This standard is applicable to any type of spacecraft including launchers, when above the atmosphere.Although spacecraft systems are clearly subject to electrical interactions while still on Earth (e. g. lightning and static electricity from handling), these aspects are not covered, since they are common to terrestrial systems and covered elsewhere. Instead this standard covers electrical effects occurring in space (i.e. from the ionosphere upwards).This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00.
Aerospace transport, Air transport, Chargings, Definitions, Electric rocket engines, Electrical, Electrical engineering, Electronic engineering, Electrostatic, Interferences, Outer space, Safety, Space probes, Space safety, Space technology, Space transport, Space vehicles, Specification, Specification (approval), Specifications, Surfaces
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