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ISO 19683 : 2017

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ISO 19683 : 2017

SPACE SYSTEMS - DESIGN QUALIFICATION AND ACCEPTANCE TESTS OF SMALL SPACECRAFT AND UNITS

International Organization for Standardization

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Table of Contents

Foreword<br>Introduction<br>1 Scope<br>2 Normative references<br>3 Terms and definitions<br>4 Abbreviated terms<br>5 General requirements<br>6 Satellite system tests<br>7 Unit tests<br>8 Test requirements<br>Annex A (normative) - Tailoring and waiver guides<br>Annex B (informative) - Basis of test levels and duration<br>Annex C (informative) - Design, verification and testing <br>&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;philosophy for small spacecrafts<br>Annex D (informative) - Test selection logic flow<br>Annex E (informative) - Environment stress screening <br>&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;and burn-in<br>Annex F (informative) - Thermal vacuum or thermal cycle?<br>Bibliography

Abstract

Gives test methods and test requirements for design qualification and/or acceptance of small spacecraft or units.

General Product Information

Document Type Standard
Status Current
Publisher International Organization for Standardization
Committee TC 20
Supersedes
  • ISO/DIS 19683 : 60.00 (2017)