ISO 15864:2004
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
View Superseded by
Space systems General test methods for space craft, subsystems and units
Hardcopy , PDF , PDF 3 Users , PDF 5 Users , PDF 9 Users
01-07-2021
English, French
10-08-2004
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ISO 15864:2004 provides the baseline standard on the subject of testing at the system, subsystem, and unit level for applicable unmanned spacecraft programs. It also provides the requirements for documentation associated with testing activities.
The acceptance criteria, specifications or procedures, and other detail test requirements applicable to a particular program are defined in the applicable technical specifications and statement of work. When requirements have to be verified by measuring product performance and function under various simulated environments, the method is referred to as "Test." The requirements of ISO 15864:2004 may be tailored for each specific space program application.
| DevelopmentNote |
Supersedes ISO/DIS 15864 (08/2004)
|
| DocumentType |
Standard
|
| Pages |
30
|
| PublisherName |
International Organization for Standardization
|
| Status |
Withdrawn
|
| SupersededBy |
| Standards | Relationship |
| BS ISO 15864:2004 | Identical |
| NBR ISO 15864 : 2007 | Identical |
| BS ISO 19924:2017 | Space systems. Acoustic testing |
| ISO 10786:2011 | Space systems — Structural components and assemblies |
| BS ISO 19683:2017 | Space systems. Design qualification and acceptance tests of small spacecraft and units |
| BS ISO 22010:2007 | Space systems. Mass properties control |
| ISO 11892:2012 | Space systems — Subsystems/units to spacecraft interface control document |
| ISO 19683:2017 | Space systems — Design qualification and acceptance tests of small spacecraft and units |
| 10/30239797 DC : 0 | BS ISO 11892 - SPACE SYSTEMS - SUBSYSTEMS/UNITS TO SPACECRAFT INTERFACE CONTROL DOCUMENT |
| BS ISO 16699:2015 | Space systems. Disposal of orbital launch stages |
| ISO 22010:2007 | Space systems — Mass properties control |
| ISO 24637:2009 | Space systems — Electromagnetic interference (EMI) test reporting requirements |
| BS ISO 16694:2015 | Space systems. The measured parameters at firing bench and flight tests of liquid rocket engines |
| ISO 19924:2017 | Space systems — Acoustic testing |
| ISO 16699:2015 | Space systems Disposal of orbital launch stages |
| BS ISO 10786:2011 | Space systems. Structural components and assemblies |
| 10/30197714 DC : 0 | BS ISO 10786 - SPACE SYSTEMS - STRUCTURAL COMPONENTS AND ASSEMBLIES |
| 13/30235921 DC : 0 | BS ISO 16694 - SPACE SYSTEMS - THE MEASURED PARAMETERS AT FIRING BENCH AND FLIGHT TESTS OF LIQUID ROCKET ENGINES |
| ISO 16694:2015 | Space systems — The measured parameters at firing bench and flight tests of liquid rocket engines |
| BS ISO 18322:2017 | Space systems. General management requirements for space test centres |
| 13/30235933 DC : 0 | BS ISO 16699 - SPACE SYSTEMS - DISPOSAL OF ORBITAL LAUNCH STAGES |
| BS ISO 11892:2012 | Space systems. Subsystems/units to spacecraft interface control document |
| 17/30311287 DC : 0 | BS ISO 19924 - SPACE SYSTEMS - ACOUSTIC TESTING |
| ISO 18322:2017 | Space systems — General management requirements for space test centres |
| 07/30146445 DC : 0 | BS ISO 24637 - SPACE SYSTEMS - ELECTROMAGNETIC INTERFERENCE (EMI) TEST REPORTING REQUIREMENTS |
| BS ISO 24637:2009 | Space systems. Electromagnetic interference (EMI) test reporting requirements |
| 16/30302535 DC : 0 | BS ISO 19683 - SPACE SYSTEMS - DESIGN QUALIFICATION AND ACCEPTANCE TESTS OF SMALL SPACECRAFT AND UNITS |
| ISO 14303:2002 | Space systems — Launch-vehicle-to-spacecraft interfaces |
| ISO 14302:2002 | Space systems Electromagnetic compatibility requirements |
| ISO 14623:2003 | Space systems - Pressure vessels and pressurized structures — Design and operation |
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