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ISO 14621-2:2003

Space systems — Electrical, electronic and electromechanical (EEE) parts — Part 2: Control programme requirements
30 korr 2003
95.99 Withdrawal of Standard   23 maj 2019

General information

95.99     23 maj 2019

ISO

ISO/TC 20/SC 14

International Standard

49.140  

anglisht   frëngjisht  

Buying

Shfuqizuar

Language in which you want to receive the document.

Scope

ISO 14621-2:2003 establishes technical guidelines for developing and documenting an electrical, electronic and electromechanical (EEE) parts control program, in order to assure that the parts used in the flight hardware are acceptable and possess adequate functional, radiation and reliability characteristics to meet the system requirements. These guidelines are tailorable to the needs of each individual programme based on the project performance criteria, risk tolerance, budget, mission duration, environment, schedule and other considerations. ISO 14621-2:2003 is applicable to all customers and suppliers furnishing flight hardware and is suitable for reference in proposal instructions.

Life cycle

NOW

WITHDRAWN
ISO 14621-2:2003
95.99 Withdrawal of Standard
23 maj 2019

REVISED BY

PUBLISHED
ISO 14621-2:2019