CEN EN 16603-32-08 Space engineering - Materials
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
- 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
- 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
- CEN EN 4700-002 Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 002: Bar and section
- 49.025.10
- 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
- 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
- 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 2213 Aerospace series - Steel FE-PL1505 (15CrMoV6) - Air melted - Hardened and tempered - Bars - De ? 16 mm - 980 MPa ? Rm ? 1 180 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
- CEN EN 4700-002 Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 002: Bar and section
- 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 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
- CEN EN 4179 Aerospace series - Qualification and approval of personnel for non-destructive testing
- 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
European Committee for Standardization
Space engineering - Materials
N EN 16603-32-08
Annotation
ECSS-E-ST-32-08 specifies the mechanical engineering requirements for materials. This Standard also encompasses the mechanical effects of the natural and induced environments to which materials used for space applications can be subjected.
This standard specifies requirements for the establishment of the mechanical and physical properties of the materials to be used for space applications, and the verification of these requirements.
Verification includes destructive and non-destructive test methods. Quality assurance requirements for materials (e.g. procurement and control) are covered by ECSS-Q-ST-70.
This standard may be tailored for the specific characteristics and constrains of a space project in conformance with ECSS-S-ST-00.
Автоматический перевод:
Космическая разработка - Материалы
ECSS E СВ. 32 08 определяет требования машиностроения для материалов. Этот Стандарт также охватывает механические эффекты естественной и вызванной окружающей среды, которой могут быть подвергнуты материалы, используемые для применения космической техники.
Этот стандарт определяет требования для учреждения механических и физических свойств материалов, которые будут использоваться для применения космической техники и проверки этих требований.
