ISO 19683:2017
p
ISO 19683:2017
66008
Indisponible en français
État actuel : Publiée (Sera révisée)
Cette norme sera remplacée parISO/AWI 19683
fr
Format Langue
std 1 208 PDF
std 2 208 Papier
  • CHF208
Convertir les francs suisses (CHF) dans une autre devise

Résumé

ISO 19683:2017 provides test methods and test requirements for design qualification and/or acceptance of small spacecraft or units. It provides the minimum test requirements and test methods to qualify the design and manufacturing methods of commercial small spacecraft and their units and to accept the final products.

ISO 19683:2017 places emphasis on achieving reliability against infant mortality after satellite launch to orbit while maintaining low cost and fast delivery.

ISO 19683:2017 is applied to satellites whose development methods are different from the ones used for traditional satellites that have little room for risk tolerance, as shown in Figure 1. The scope of this document encompasses different categories of small spacecraft, so-called mini-, micro, nano-, pico- and femto-, as well as CubeSat, spacecraft. Therefore, for the sake of convenience, the term "small spacecraft" is used throughout this document as a generic term.

ISO 19683:2017 includes CubeSat, as long as it is developed with the untraditional processes.

Informations générales

  •  : Publiée
     : 2017-07
    : Norme internationale à réviser [90.92]
  •  : 1
  • ISO/TC 20/SC 14
    49.140 
  • RSS mises à jour

Prévisualiser 

Prévisualiser cette norme sur notre Plateforme de consultation en ligne (OBP)

Vous avez une question?

Consulter notre FAQ

Service à la clientèle
+41 22 749 08 88

Horaires d’ouverture:
De lundi à vendredi - 09:00-12:00, 14:00-17:00 (UTC+1)