ISO 24113 Space systems — Space debris mitigation requirements - Second Edition
Данный раздел/документ содержится в продуктах:
- Техэксперт: Машиностроительный комплекс
- Картотека зарубежных и международных стандартов
- ISO 24113 Space systems — Space debris mitigation requirements - First Edition
- 49
- ISO 24113 Space systems — Space debris mitigation requirements - First Edition
- 49.140
- ISO 23339 Space systems — Unmanned spacecraft — Estimating the mass of remaining usable propellant - First Edition
- ISO 23339 Space systems — Unmanned spacecraft — Estimating the mass of remaining usable propellant - First Edition
- ISO 27875 Space systems - Re-entry risk management for unmanned spacecraft and launch vehicle orbital stages - First Edition
- ISO 16164 Space Systems - Disposal of satellites operating in or crossing Low Earth Orbit - First Edition
- ISO 27852 Space systems — Estimation of orbit lifetime - First Edition
- Картотека зарубежных и международных стандартов
International Organization for Standardization
Space systems — Space debris mitigation requirements - Second Edition
N 24113
Annotation
This International Standard defines the primary space debris mitigation requirements applicable to all elements of unmanned systems launched into, or passing through, near-Earth space, including launch vehicle orbital stages, operating spacecraft and any objects released as part of normal operations or disposal actions.
The requirements contained in this International Standard are intended to reduce the growth of space debris by ensuring that spacecraft and launch vehicle orbital stages are designed, operated and disposed of in a manner that prevents them from generating debris throughout their orbital lifetime.
This International Standard is the top-level standard in a family of standards addressing debris mitigation. It will be the main interface for the user, bridging between the primary debris mitigation requirements and the lower-level implementation standards that will ensure compliance.
This International Standard does not cover launch phase safety for which specific rules are defined elsewhere.
Автоматический перевод:
Космические системы — требования смягчения Космических обломков - Второй Выпуск
Этот Международный эталон определяет основные требования смягчения космических обломков, применимые ко всем элементам беспилотных систем, начал, или пропускание, околоземное пространство, включая ракету-носитель орбитальные стадии, операционный космический корабль и любые объекты, выпущенные как часть действий распоряжения или штатных функционирований.



