CEN EN 16602-70-04 Space product assurance - Thermal testing for the evaluation of space materials, processes, mechanical parts and assemblies
Данный раздел/документ содержится в продуктах:
- Техэксперт: Машиностроительный комплекс
- Картотека зарубежных и международных стандартов
- CEN EN 16602-70-29 Space product assurance - Determination of offgassing products from materials and assembled articles to be used in a manned space vehicle crew compartment
- 49
- CEN EN 16602-70-29 Space product assurance - Determination of offgassing products from materials and assembled articles to be used in a manned space vehicle crew compartment
- 49.140
- CEN EN 16602-70-29 Space product assurance - Determination of offgassing products from materials and assembled articles to be used in a manned space vehicle crew compartment
- DIN EN 16602-20-07 Space produce assurance - Quality and safety assurance for space test centres
- DIN EN 16602-20-07 Space produce assurance - Quality and safety assurance for space test centres
- DIN EN 16602-20-07 Space produce assurance - Quality and safety assurance for space test centres
- DIN EN 16602-20-08 Space product assurance - Storage, handling and transportation of spacecraft hardware
- DIN EN 16602-70 Space product assurance - Materials, mechanical parts and processes
- DIN EN 16602-70-71 Space product assurance - Materials, processes and their data selection
- DIN EN 16602-70-10 Space product assurance - Qualification of printed circuit boards
- CEN EN 16602-20 Space product assurance - Quality assurance
- Картотека зарубежных и международных стандартов
European Committee for Standardization
Space product assurance - Thermal testing for the evaluation of space materials, processes, mechanical parts and assemblies
N EN 16602-70-04
Annotation
This Standard establishes the requirements for the specification, the procedures, the execution and the reporting of a thermal cycling test under vacuum for the evaluation of materials, processes, mechanical parts and assemblies intended for use in the fabrication of spacecraft and associated equipment. This is one of the tests to determine the ability of theses articles to withstand changes of ambient temperature under vacuum.
Typical materials or assemblies that can be evaluated by means of this test method are listed below.
- adhesives;
- adhesive bonded joints;
- coatings (paint, thermal and protective);
- insulating materials;
- metallic bonded joints;
- metallic samples, finished by plating or chemical conversion;
- metallized plastic films;
- organic or nonorganic bonding;
- plated surfaces;
- potting compounds;
- reinforced structural laminates;
- sealants.
NOTE This is not an exhaustive list and other products or items can be tested.
This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00.



