GB/T 34513-2017 in English
VALIDSpace debris mitigation requirements
- Issued on:2017-11-01
- Implemented on:2018-05-01
- File Format:PDF
- Delivery:Via email within 1~3 business days
$175.00
《GB/T 34513-2017空间碎片减缓要求》由TC425(全国宇航技术及其应用标准化技术委员会)归口,TC425SC5(全国宇航技术及其应用标准化技术委员会空间碎片分会)执行,主管部门为国家标准化管理委员会。
Introduction
Overview of the Space Debris Mitigation Standard Framework
| Dimensions | ISO 24113:2011 | GB/T 34513-2017 | Difference Analysis |
|---|---|---|---|
| Scope of Application | All space systems entering or passing through near-Earth space | Same as above | No difference |
| Definition of Protected Areas | LEO and GEO areas | Same as above | Terminology consistency maintained |
| Technical Requirements | Avoiding intentional release of debris, on-orbit disintegration control, and post-mission disposal | Specific calculation methods to increase the probability of successful disposal | Detailed requirements |
Professional terms and practical application cases
Probability of successful disposal: refers to the probability that a spacecraft or launch vehicle orbital stage successfully completes the disposal action after the mission is completed. For example, in Case 1, if the nominal mission success probability is 90%, P(D|M) can be calculated as:
P(D|M) = [R_system(T_mission + T_disposal)] / R_system(T_mission)] * P_propellant
Standard formulation background and technology evolution analysis
With the increasing frequency of space activities, the issue of space debris has become a focus of global attention. The International Telecommunication Union (ITU), the Inter-Agency Space Debris Coordination Committee (IADC) and the United Nations (UN) have all issued relevant guidelines. ISO has translated these consensuses into specific standards, promoting more standardized design and operation of space systems.
Implementation recommendations
- Design phase: Ensure that spacecraft and launch vehicle orbital stages do not release debris into Earth orbit during normal operation, paying special attention to the size control of combustion products.
- On-orbit management: Avoid accidental disintegration events, regularly monitor the status of the spacecraft, and ensure that it is disposed of before the end of its life.
- Post-mission phase: Depending on the specific orbital position (LEO or GEO), take appropriate measures to move the spacecraft out of the protected area, such as controlled reentry or orbital maneuvers.

Loading PDF document...
Error loading PDF. Please make sure the file is valid and try again.
We also recommend
-

GB/T 44316-2024 in English
Space objects observation data specification
2024-08-23 -

GB/T 47037-2026 in English
Space data and information transfer systems—Delta-DOR raw data exchange format
2026-01-28 -

GB/T 46527-2025 in English
Space data and information transfer systems—Operation of CFDP over encapsulation service
2025-10-31