BS ISO 19933:2007
Current
The latest, up-to-date edition.
Space systems. Format for spacecraft launch environment test report
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.
Committee |
ACE/68
|
DevelopmentNote |
Supersedes 06/30140973 DC. (01/2008)
|
DocumentType |
Standard
|
PublisherName |
British Standards Institution
|
Status |
Current
|
Supersedes |
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:
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static load;
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modal survey;
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sine vibration;
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acoustic noise;
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random vibration;
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shock; and
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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.
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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