DIN EN 16603-31 Space engineering - Thermal control general requirements; English version EN 16603-31:2014
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
- 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
- DIN EN 16603-34 Space engineering - Part 34: Environmental control and life support (ECLS)
- Картотека зарубежных и международных стандартов
Deutsches Institut fur Normung e. V.
Space engineering - Thermal control general requirements; English version :2014
N EN 16603-31
Annotation
ECSS-E-ST-31 defines requirements for the discipline of thermal engineering.
This Standard defines the requirements for the definition, analysis, design, manufacture, verification and in-service operation of thermal control subsystems of spacecraft and other space products.
For this Standard, the complete temperature scale is divided into three ranges:
• Cryogenic temperature range
• Conventional temperature range
• High temperature range.
The requirements of this Standard are applicable to the complete temperature scale. However, where applicable, requirements are stated to be applicable only for the cryogenic or high temperature range. References to these specific requirements have been summarized in Annex G and Annex H.
This standard is applicable to all flight hardware of space projects, including spacecraft and launchers.
This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00.
Автоматический перевод:
Космическая техника - Терморегуляция общие требования; английская версия 16603-31:2014 EN
