DIN EN 16602-70-04 Space product assurance - Thermal testing for the evaluation of space materials, processes, mechanical parts and assemblies; English version EN 16602-70-04:2014
Данный раздел/документ содержится в продуктах:
- Техэксперт: Машиностроительный комплекс
- Картотека зарубежных и международных стандартов
- DIN EN 4656 Aerospace series - Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bars - a or D ? 200 mm - Rm ? 1520 MPa
- CEN EN 4700-002 Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 002: Bar and section
- DIN EN 4720 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electroslag remelted (ESR) - Hardened and tempered - Bar - De ? 200 mm - 1150 MPa ? Rm ? 1300 MPa
- DIN EN 4050-4 Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 4: Acceptance criteria
- DIN EN 4050-1 Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 1: General requirements
- DIN EN 4050-4 Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 4: Acceptance criteria
- DIN EN 4720 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electroslag remelted (ESR) - Hardened and tempered - Bar - De ? 200 mm - 1150 MPa ? Rm ? 1300 MPa
- CEN EN 4700-002 Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 002: Bar and section
- 49
- DIN EN 4656 Aerospace series - Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bars - a or D ? 200 mm - Rm ? 1520 MPa
- CEN EN 4700-002 Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 002: Bar and section
- DIN EN 4720 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electroslag remelted (ESR) - Hardened and tempered - Bar - De ? 200 mm - 1150 MPa ? Rm ? 1300 MPa
- DIN EN 4050-4 Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 4: Acceptance criteria
- DIN EN 4050-1 Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 1: General requirements
- DIN EN 4050-4 Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 4: Acceptance criteria
- DIN EN 4720 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electroslag remelted (ESR) - Hardened and tempered - Bar - De ? 200 mm - 1150 MPa ? Rm ? 1300 MPa
- CEN EN 4700-002 Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 002: Bar and section
- 49.025
- DIN EN 4656 Aerospace series - Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bars - a or D ? 200 mm - Rm ? 1520 MPa
- CEN EN 4700-002 Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 002: Bar and section
- DIN EN 4720 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electroslag remelted (ESR) - Hardened and tempered - Bar - De ? 200 mm - 1150 MPa ? Rm ? 1300 MPa
- DIN EN 4050-4 Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 4: Acceptance criteria
- DIN EN 4050-1 Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 1: General requirements
- DIN EN 4050-4 Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 4: Acceptance criteria
- DIN EN 4720 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electroslag remelted (ESR) - Hardened and tempered - Bar - De ? 200 mm - 1150 MPa ? Rm ? 1300 MPa
- CEN EN 4700-002 Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 002: Bar and section
- DIN EN 4656 Aerospace series - Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bars - a or D ? 200 mm - Rm ? 1520 MPa
- DIN EN 4656 Aerospace series - Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bars - a or D ? 200 mm - Rm ? 1520 MPa
- CEN EN 4700-002 Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 002: Bar and section
- DIN EN 4720 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electroslag remelted (ESR) - Hardened and tempered - Bar - De ? 200 mm - 1150 MPa ? Rm ? 1300 MPa
- DIN EN 4050-4 Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 4: Acceptance criteria
- DIN EN 4050-1 Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 1: General requirements
- DIN EN 4050-4 Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 4: Acceptance criteria
- DIN EN 4720 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electroslag remelted (ESR) - Hardened and tempered - Bar - De ? 200 mm - 1150 MPa ? Rm ? 1300 MPa
- DIN EN 4720 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electroslag remelted (ESR) - Hardened and tempered - Bar - De ? 200 mm - 1150 MPa ? Rm ? 1300 MPa
- DIN EN 4050-4 Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 4: Acceptance criteria
- DIN EN 4050-1 Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 1: General requirements
- DIN EN 4050-4 Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 4: Acceptance criteria
- DIN EN 4050-4 Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 4: Acceptance criteria
- DIN EN 4050-1 Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 1: General requirements
- DIN EN 4050-1 Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 1: General requirements
- CEN EN 4179 Aerospace series - Qualification and approval of personnel for non-destructive testing
- CEN EN 16603-32-08 Space engineering - Materials
- CEN EN 16602-70-71 Space product assurance - Materials, processes and their data selection
- DIN EN 16602-70-12 Space product assurance - Design rules for printed circuit boards
- DIN EN 16602-70-71 Space product assurance - Materials, processes and their data selection
- DIN EN 16602-70 Space product assurance - Materials, mechanical parts and processes
- DIN EN 4656 Aerospace series - Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bars - a or D ? 200 mm - Rm ? 1520 MPa
- Картотека зарубежных и международных стандартов
Deutsches Institut fur Normung e. V.
Space product assurance - Thermal testing for the evaluation of space materials, processes, mechanical parts and assemblies; English version :2014
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.



