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ILNAS-EN 16603-20-21:2020 Edition 06/2020
Space engineering - Interface requirements for electrical actuators
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Abstract

In general terms, the scope of the consolidation of the electrical interface requirements for electrical (hold down and release or deployment) actuators in the present ECSS-E-ST-20-21 and the relevant explanation in the handbook ECSS-E-HB-20-21 is to allow a more recurrent approach both for actuator electronics (power source) and electrical actuators (power load) offered by the relevant manufacturers, at the benefit of the system integrators and of the Agency, thus ensuring: - better quality, - stability of performances, and - independence of the products from specific mission targets. A recurrent approach enables manufacturing companies to concentrate on products and a small step improvement approach that is the basis of a high quality industrial output.

Status

Standard - Active

Origin

Technical Committee :
CEN/CLC/JTC 5 : Space

Implementation

start of the vote on the project    05/09/2019   date of ratification (dor)    24/05/2020
end of the vote on the project    28/11/2019   date of anouncement (doa)    30/09/2020
start of the vote on the final project    27/02/2020   date of publication (dop)    31/12/2020
end of the vote on the final project    23/04/2020   date of withdrawal (dow)    31/12/2020


Publication Official Journal
of the Grand-Duchy of Luxembourg
24/12/2020
Reference Mémorial A N° 1077

International Classification for Standards (ICS codes) :

49.140 : Space systems and operations

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