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space debris mitigation requirements introduction overview space debris space debris mitigation standard framework dimensions iso successful disposal detailed requirements inter-agency space debris coordination committee frame-type walking frames grain warehouse androgen drug residues
GB/T 34513-2017 in English

GB/T 34513-2017 in English

VALID

Space debris mitigation requirements

  • Issued on:2017-11-01
  • Implemented on:2018-05-01
  • File Format:PDF
  • Delivery:Via email within 1~3 business days
Price(USD): $180.00
$175.00
Standard No: GB/T 34513-2017
Document status: VALID
Superseded by: GB/T 34513-2026 Space debris mitigation requirements
Superseded on: 2026-11-01
Title in English: Space debris mitigation requirements
Title in Chinese: 空间碎片减缓要求
Language: English
File Format: Electronic (PDF)
Delivery: Via email within 1~3 business days
Issued on: 2017-11-01
Implemented on: 2018-05-01
ICS Classification: 49.140-Space systems and operations
Chinese Classification: V70-Spacecraft in general
Professional Classification: GB-National Standard
Related Keywords: space debris mitigation requirements introduction overview
space debris
space debris mitigation standard framework dimensions iso
successful disposal detailed requirements
inter-agency space debris coordination committee
Related Topics: Fragmentation
space debris
fragments
debris peak
debris peak
space debris
space debris
slow down
secondary debris
Space Debris Detection
relief time
Secondary Fragment English
earth space debris
GBT34513
GB/T 34513-2017

《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

  1. 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.
  2. 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.
  3. 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.

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