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BS EN 16603-10-03:2022

BS EN 16603-10-03:2022

$215.11

Space engineering. Testing

Published By Publication Date Number of Pages
BSI 2022 136
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PDF Pages PDF Title
2 undefined
11 1 Scope
13 2 Normative references
14 3 Terms, definitions and abbreviated terms
3.1 Terms from other standards
15 3.2 Terms specific to the present standard
21 3.3 Abbreviated terms
24 3.4 Nomenclature
25 4 General requirements
4.1 Test programme
4.2 Development test prior qualification
26 4.3 Test management
4.3.1 General
4.3.2 Test reviews
4.3.2.1 Test programme
27 4.3.2.2 Test readiness review (TRR)
28 4.3.2.3 Post test review (PTR)
29 4.3.2.4 Test review board (TRB)
30 4.3.3 Test documentation
4.3.3.1 General
4.3.3.2 Assembly, integration and test plan (AIT Plan)
4.3.3.3 Test specification (TSPE)
4.3.3.4 Test procedure (TPRO)
31 4.3.3.5 Test report (TRPT)
4.3.4 Anomaly or failure during testing
4.3.5 Test data
4.4 Test conditions, input tolerances, and measurement uncertainties
4.4.1 Test conditions
32 4.4.2 Test input tolerances
34 4.4.3 Measurement uncertainties
36 4.5 Test objectives
4.5.1 General requirements
4.5.2 Qualification testing
37 4.5.3 Acceptance testing
4.5.4 Protoflight testing
4.5.4.1 Overview
4.5.4.2 Requirements
38 4.6 Retesting
4.6.1 Overview
4.6.2 Implementation of a design modification after completion of qualification
4.6.3 Storage after protoflight or acceptance testing
39 4.6.4 Space segment element or equipment to be re-flown
40 4.6.5 Flight use of qualification Space segment element or equipment
41 5 Space segment equipment test requirements
5.1 General requirements
44 5.2 Qualification tests requirements
53 5.3 Acceptance test requirements
60 5.4 Protoflight test requirements
68 5.5 Space segment equipment test programme implementation requirements
5.5.1 General tests
5.5.1.1 Functional and performance tests
69 5.5.1.2 Humidity test
70 5.5.1.3 Life test
71 5.5.1.4 Burn-in test
5.5.2 Mechanical tests
5.5.2.1 Physical properties measurements
72 5.5.2.2 Acceleration test (static, spin or sine burst)
5.5.2.3 Random vibration test
5.5.2.4 Acoustic test
73 5.5.2.5 Sinusoidal vibration test
5.5.2.6 Shock test
74 5.5.2.7 Micro-vibration generated environment test
5.5.2.8 Micro-vibration susceptibility test
75 5.5.3 Structural integrity under pressure tests
5.5.3.1 Leak test
76 5.5.3.2 Proof pressure test
5.5.3.3 Pressure cycling test
5.5.3.4 Design burst pressure test
5.5.3.5 Burst test
5.5.4 Thermal tests
5.5.4.1 Requirements applicable to thermal vacuum test and thermal test at mission pressure
78 5.5.4.2 Requirements applicable to thermal vacuum test
5.5.4.3 Requirements applicable to thermal test at mission pressure
79 5.5.5 Electrical/RF tests
5.5.5.1 EMC test
5.5.5.2 Magnetic test
5.5.5.3 ESD test
5.5.5.4 Passive intermodulation test
80 5.5.5.5 Multipactor test
5.5.5.6 Corona and arc discharge test
5.5.6 Mission specific test
5.5.6.1 Audible noise test
81 6 Space segment element test requirements
6.1 General requirements
6.2 Qualification test requirements
89 6.3 Acceptance test requirements
96 6.4 Protoflight test requirements
103 6.5 Space segment elements test programme implementation requirements
6.5.1 General tests
6.5.1.1 Optical alignment measurement
6.5.1.2 Functional tests
105 6.5.1.3 Performance test
6.5.1.4 Mission test
106 6.5.1.5 Polarity test
107 6.5.1.6 Launcher interface test
6.5.2 Mechanical tests
6.5.2.1 Physical properties measurements
108 6.5.2.2 Modal survey test
6.5.2.3 Static load test
6.5.2.4 Spin test
6.5.2.5 Transient and Sine Burst Tests
109 6.5.2.6 Acoustic test
110 6.5.2.7 Random vibration test
6.5.2.8 Sinusoidal vibration test
111 6.5.2.9 Shock test
112 6.5.2.10 Micro-vibration susceptibility test
113 6.5.2.11 Micro-vibration emission test
6.5.3 Structural integrity under pressure tests
6.5.3.1 Proof pressure test
6.5.3.2 Pressure cycling test
6.5.3.3 Design burst pressure test
114 6.5.3.4 Leak test
6.5.4 Thermal tests
6.5.4.1 Requirements applicable to thermal vacuum test and thermal tests at mission pressure
115 6.5.4.2 Requirements applicable to thermal vacuum test
6.5.4.3 Requirements applicable to thermal test at mission pressure
116 6.5.4.4 Thermal balance test
6.5.5 Electromagnetic tests
6.5.5.1 General
6.5.5.2 Electromagnetic compatibility test
6.5.5.3 Electromagnetic auto-compatibility test
117 6.5.5.4 Passive intermodulation test
6.5.5.5 Magnetic field measurements
6.5.6 Mission specific tests
6.5.6.1 Aero-thermodynamic test
6.5.7 Crewed mission specific tests
6.5.7.1 Vibroacoustic emission test
118 6.5.7.2 Human factor engineering (HFE) test
6.5.7.3 Toxic off gassing test
6.5.7.4 Audible noise test
119 7 Pre-launch testing

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BS EN 16603-10-03:2022
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