BS ISO 24412:2023
$167.15
Space systems. Thermal vacuum environmental testing
Published By | Publication Date | Number of Pages |
BSI | 2023 | 40 |
PDF Catalog
PDF Pages | PDF Title |
---|---|
2 | National foreword |
7 | Foreword |
8 | Introduction |
9 | 1 Scope 2 Normative references 3 Terms and definitions |
10 | 4 Symbols and abbreviated terms 5 Test purpose 5.1 Thermal balance test |
11 | 5.2 Thermal vacuum test 5.2.1 General purpose 5.2.2 Qualification test 5.2.3 Proto-flight test 5.2.4 Acceptance test 6 Test methods 6.1 Thermal balance test 6.1.1 Test description |
14 | 6.1.2 Test conditions |
15 | 6.1.3 Basic requirements of test facilities 6.1.4 Monitoring during TBT 6.2 Thermal vacuum test 6.2.1 Test description |
18 | 6.2.2 Test conditions |
21 | 6.2.3 Basic requirements for test facilities 6.2.4 Monitoring during TVT 7 Test facility 7.1 Laboratory environment |
22 | 7.2 Laboratory infrastructure 7.3 Test system 7.3.1 Overview 7.3.2 Chamber system |
23 | 7.3.3 Vacuum system 7.3.4 Thermal system |
26 | 7.3.5 Data acquisition system 7.3.6 MGSE 7.3.7 Contamination measurement and control system |
27 | 8 Test requirements 8.1 Test tolerance and accuracy |
28 | 8.2 Test configuration 8.3 Temperature and heat flux measurement 8.3.1 General 8.3.2 Location of temperature monitoring point for test article 8.3.3 Location of temperature monitoring point for test equipment |
29 | 8.4 Heating device selection 8.5 Safety requirements and recommendations 9 Test procedure 9.1 Test flow |
30 | 9.2 Test procedure 9.2.1 General 9.2.2 Before test |
31 | 9.2.3 Test implementation 9.2.4 After test |
32 | 10 Test interruption and handling 10.1 Interruption 10.1.1 Test facility malfunction 10.1.2 Test article malfunction 10.2 Interruption handling |
33 | 11 Test documentation |
34 | Annex A (informative) Main characteristic of a solar simulator |
36 | Annex B (informative) An example of IR heater design flow for absorbed flux simulation method in TBT |
39 | Bibliography |