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BS ISO 19933:2007

Current

Current

The latest, up-to-date edition.

Space systems. Format for spacecraft launch environment test report

Published date

31-12-2007

Foreword
Introduction
1 Scope
2 Normative references
3 Terms, definitions and abbreviated terms
   3.1 Terms and definitions
   3.2 Abbreviated terms
4 Introduction section of a test report
   4.1 General
   4.2 Overall test sequence
5 Referenced documentation section of a test report
   5.1 general
   5.2 Normative references
   5.3 Applicable references
   5.4 Informative references
6 Nomenclature section of a test report
7 Test objective section of a test report
   7.1 General
   7.2 Test strategy matrix
8 Test article configuration section of a test report
   8.1 General
   8.2 Identification and general configuration matrix
   8.3 Deviations from flight configuration
   8.4 Functional configuration
9 Test facility configuration section of a test report
   9.1 General
   9.2 Test configuration
   9.3 Test facility constraints and limitations
10 Test description section of a test report
   10.1 General
   10.2 Test approach and methodology
   10.3 Test flow
   10.4 Supporting analyses
   10.5 Input parameters, tolerances and limits
   10.6 Instrumentation
   10.7 Success criteria
11 Test results section of test reports
   11.1 Static load
   11.2 Modal survey
   11.3 Sine vibration
   11.4 Acoustic noise
   11.5 Random vibration
   11.6 Shocks
   11.7 Electromagnetic compatibility
12 Test result evaluation section of a test report
13 Test deviations section of a test report
14 Test conclusion section of a test report
Bibliography

Describes format to report the test process and results of spacecraft (SC) qualification to the launch environment.

This International Standard provides a specific format to report the test process and results of spacecraft (SC) qualification to the launch environment. The following types of tests are considered:

  • static load;

  • modal survey;

  • sine vibration;

  • acoustic noise;

  • random vibration;

  • shock; and

  • electromagnetic compatibility (EMC).

The definition of test specifications and test requirements are derived from launch vehicle (LV) user’s manuals as defined in ISO14303. Only those tests that are intended to demonstrate the compliance of a given SC design with its LV environment are taken into consideration.

Committee
ACE/68
DevelopmentNote
Supersedes 06/30140973 DC. (01/2008)
DocumentType
Standard
PublisherName
British Standards Institution
Status
Current
Supersedes

Standards Relationship
ISO 19933:2007 Identical

ISO 14303:2002 Space systems — Launch-vehicle-to-spacecraft interfaces
ISO 15863:2003 Space systems Spacecraft-to-launch-vehicle interface control document
ISO 17566:2011 Space systems General test documentation

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