GB/T 45741-2025
ActiveLifetime estimation method of space debris in low earth orbit
低地球轨道空间碎片寿命计算方法
Application Summary AI generated
This standard specifies a method for estimating the orbital lifetime of space debris objects in low Earth orbit (LEO), accounting for atmospheric drag, solar activity, and gravitational perturbations. It is applied by spacecraft designers, mission planners, and space agencies to assess debris decay timelines for collision risk analysis and post-mission disposal compliance. The standard supports debris mitigation efforts in the aerospace industry, particularly for satellites and rocket bodies operating between 200 km and 2,000 km altitude.
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Transparency note: The application summary and key sentences on this page were automatically generated by AI from the standard's original text. This content has not been human-verified and should not be used for compliance or regulatory purposes. Always refer to the official standard document from the issuing authority.