CEN EN 16603-32 Space engineering - Structural general requirements
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 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 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 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
- 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
- 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 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 4050-4 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
- CEN EN 16603-32-08 Space engineering - Materials
- 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 - Structural general requirements
N EN 16603-32
Annotation
ECSS-E-ST-32C (Space engineering – Structural) defines the mechanical engineering requirements for structural engineering.
This Standard specifies the requirements to be considered in all engineering aspects of structures: requirement definition and specification, design, development, verification, production, inservice and eventual disposal.
The Standard applies to all general structural subsystem aspects of space products including: launch vehicles, transfer vehicles, reentry vehicles, spacecraft, landing probes and rovers, sounding rockets, payloads and instruments, and structural parts of all subsystems.
This Standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S-ST-00.
Автоматический перевод:
Космическая техника - Структурные общие требования
ECSS E СВ. 32C (Космическая техника – Структурный) определяет требования машиностроения для структурной разработки.
Этот Стандарт определяет требования, которые рассмотрят во всех технических аспектах структур: определение требования и спецификация, дизайн, развитие, проверка, производство, штатное и возможное распоряжение.
