ISO 16290:2013
Space systems — 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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Section sec_1
Section sec_2
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Table tab_1
Reference ref_1
Foreword
Introduction
1 Scope
2 Terms and definitions
3 Technology Readiness Levels (TRLs)
3.1 General
3.2 TRL 1 — Basic principles observed and reported
3.3 TRL 2 — Technology concept and/or application formulated
3.4 TRL 3 — Analytical and experimental critical function and/or characteristic proof-of-concept
3.5 TRL 4 — Component and/or breadboard functional verification in laboratory environment
3.6 TRL 5 — Component and/or breadboard critical function verification in a relevant environment
3.7 TRL 6 — Model demonstrating the critical functions of the element in a relevant environment
3.8 TRL 7 — Model demonstrating the element performance for the operational environment
3.9 TRL 8 — Actual system completed and accepted for flight (“flight qualified”)
3.10 TRL 9 — Actual system “flight proven” through successful mission operations
4 Summary table
Bibliography
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Section sec_1
Section sec_2
Section sec_2.1
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Section sec_2.4
Section sec_2.5
Section sec_2.6
Section sec_2.7
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Section sec_2.21
Section sec_3
Section sec_3.1
Section sec_3.2
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Section sec_3.2.2
Section sec_3.3
Section sec_3.3.1
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Section sec_3.4
Section sec_3.4.1
Section sec_3.4.2
Section sec_3.5
Section sec_3.5.1
Section sec_3.5.2
Section sec_3.6
Section sec_3.6.1
Section sec_3.6.2
Section sec_3.7
Section sec_3.7.1
Section sec_3.7.2
Section sec_3.8
Section sec_3.8.1
Section sec_3.8.2
Section sec_3.9
Section sec_3.9.1
Section sec_3.9.2
Section sec_3.10
Section sec_3.10.1
Section sec_3.10.2
Section sec_4
Table tab_1
Reference ref_1
Foreword
Introduction
1 Scope
2 Terms and definitions
3 Technology Readiness Levels (TRLs)
3.1 General
3.2 TRL 1 — Basic principles observed and reported
3.3 TRL 2 — Technology concept and/or application formulated
3.4 TRL 3 — Analytical and experimental critical function and/or characteristic proof-of-concept
3.5 TRL 4 — Component and/or breadboard functional verification in laboratory environment
3.6 TRL 5 — Component and/or breadboard critical function verification in a relevant environment
3.7 TRL 6 — Model demonstrating the critical functions of the element in a relevant environment
3.8 TRL 7 — Model demonstrating the element performance for the operational environment
3.9 TRL 8 — Actual system completed and accepted for flight (“flight qualified”)
3.10 TRL 9 — Actual system “flight proven” through successful mission operations
4 Summary table
Bibliography