NF ISO 16290

NF ISO 16290

December 2014
Standard Current

Space system - Definition of the technology readiness levels (TRLs) and their criteria of assessment

ISO 16290:2013 defines Technology Readiness Levels (TRLs). It is applicable primarily to space system hardware, although the definitions could be used in a wider domain in many cases.The definition of the TRLs provides the conditions to be met at each level, enabling accurate TRL assessment.

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Main informations

Collections

National standards and national normative documents

Publication date

December 2014

Number of pages

18 p.

Reference

NF ISO 16290

ICS Codes

49.140   Space systems and operations

Classification index

L90-118

Print number

1

International kinship

ISO 16290:2013
Sumary
Space system - Definition of the technology readiness levels (TRLs) and their criteria of assessment

ISO 16290:2013 defines Technology Readiness Levels (TRLs). It is applicable primarily to space system hardware, although the definitions could be used in a wider domain in many cases.

The definition of the TRLs provides the conditions to be met at each level, enabling accurate TRL assessment.

Table of contents
  • Avant-propos
    iv
  • Introduction
    v
  • 1 Domaine d'application
    1
  • 2 Termes et définitions
    1
  • 3 Niveaux de maturité technologique (TRLs)
    4
  • 3.1 Généralités
    4
  • 3.2 TRL 1- Principes de base observés et rapportés
    5
  • 3.3 TRL 2 - Concept technologique et/ou application formulés
    6
  • 3.4 TRL 3 - Preuve du concept analytique et expérimentale de la fonction et/ou de la caractéristique critique
    6
  • 3.5 TRL 4 - Vérification fonctionnelle en environnement de laboratoire au niveau composant et/ou maquette
    7
  • 3.6 TRL 5 - Vérification en environnement représentatif de la fonction critique au niveau composant et/ou maquette
    7
  • 3.7 TRL 6 - Démonstration en environnement représentatif des fonctions critiques de l'élément au niveau modèle
    8
  • 3.8 TRL 7 - Démonstration en environnement opérationnel de la performance de l'élément au niveau modèle
    9
  • 3.9 TRL 8 - Système réel développé et accepté pour le vol ("qualifié vol")
    10
  • 3.10 TRL 9 - Système réel « démontré en vol » par mission opérationnelle réussie
    10
  • 4 Tableau récapitulatif
    11
  • Bibliographie
    13
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