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ISO 17851:2016 Space systems - Space environment simulation for material tests - General principles and criteria >
ISO 17851:2016 Space systems - Space environment simulation for material tests - General principles and criteria, 2016
- Foreword
- Introduction
- 1 Scope
- 2 Normative references
- 3 Terms and definitions
- 3.1 Terms related to regions in space
- 3.2 Terms related to orbits
- 3.3 Terms related to space environment factors affecting spacecrafts
- 3.4 Terms related to penetration depth of affecting space factors
- 3.5 Terms related to physical and chemical mechanisms of space environment effects on materials
- 4 Abbreviated terms and symbols
- 4.1 Abbreviated terms
- 4.2 Symbols
- 5 Choice of sets of space environment components for typical orbits and regions of space
- 5.1 LEO, including polar (Sun synchronous) orbits
- 5.2 MEO
- 5.3 GSO/GEO
- 5.4 Interplanetary space
- 5.5 Moon
- 5.6 Mars
- 5.7 Jupiter
- 5.8 Mercury
- 5.9 Venus
- 6 General processes for simulation of space environment impact on materials
- 6.1 Processes for simulation
- 6.1.1 LEO including polar orbits
- 6.1.2 MEO
- 6.1.3 GSO/GEO
- 6.1.4 Interplanetary space
- 6.1.5 Near-Moon space and on the Moon surface
- 6.1.6 Near-Mars space and on the Martian surface
- 6.1.7 Near-Jupiter space
- 6.1.8 Near-Mercury and on its surface
- 6.1.9 Near-Venus space and on the Venusian surface
- 6.2 Setting a problem of simulation of space environment on spacecraft materials
- 6.3 Principles of ground-based tests
- 6.4 Requirements to physical and mathematical models
- 6.5 Choice of parameters of laboratory facilities
- 7 General criteria of material resistance to space environment
- 7.1 General regulations on testing materials to space environment
- 7.2 Functional purpose of spacecraft materials
- 7.3 UV tests
- 7.3.1 Degradation mechanism
- 7.3.2 UV sensitive materials
- 7.3.3 Limitations of ground test
- 7.3.4 Typical test apparatus
- 7.3.5 Reference test standards
- 7.4 VUV tests
- 7.4.1 Degradation mechanism
- 7.4.2 VUV sensitive materials
- 7.4.3 Limitations of ground test
- 7.4.4 Typical test apparatus
- 7.4.5 Reference test standards
- 7.5 AO tests
- 7.5.1 Degradation mechanism
- 7.5.2 AO sensitive materials
- 7.5.3 Limitations of ground test
- 7.5.4 Typical test apparatus
- 7.5.5 Reference test standards
- 7.6 Outgassing tests
- 7.6.1 Degradation mechanism
- 7.6.2 Thermal vacuum sensitive materials
- 7.6.3 Limitations of ground test
- 7.6.4 Typical test apparatus
- 7.6.5 Reference test standards
- 7.7 Thermal cycling tests
- 7.7.1 Degradation mechanism
- 7.7.2 Thermal cycling sensitive materials
- 7.7.3 Limitations of ground test
- 7.7.4 Typical test apparatus
- 7.7.5 Reference test standards
- 7.8 Radiation tests
- 7.8.1 Degradation mechanism
- 7.8.2 Radiation sensitive materials
- 7.8.3 Limitations of ground test
- 7.8.4 Typical test apparatus
- 7.8.5 Reference test standards
- 7.9 Micrometeoroid tests
- 7.9.1 Degradation mechanism
- 7.9.2 Hypervelocity impact sensitive materials
- 7.9.3 Limitations of ground test
- 7.9.4 Typical test apparatus
- 7.9.5 Reference test standards
- 8 Recommendations for simulating action of space environment on materials
- 9 Outlook for usage of this International Standard
- Annex A (informative) Space environment factors, their main parameters and effects
- Annex B (informative) Mathematical models for research of spacecraft/environment interaction
- Bibliography [Go to Page]