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earth orbit environment introduction analysis orbit altitude 1000-5000km orbit synchronous orbit geostationary orbit lodometric method scopethis standard bridge navigation safety impact demonstration report golf industry
GB/T 41542-2022 in English

GB/T 41542-2022 in English

VALID

General specification of observation elements for Earth orbit environment

  • Issued on:2022-07-11
  • Implemented on:2023-02-01
  • File Format:PDF
  • Delivery:Via email within 1~3 business days
Price(USD): $160.00
$156.00

《GB/T 41542-2022地球卫星轨道空间环境探测要素通用规范》由TC312(全国空间科学及其应用标准化技术委员会)归口,主管部门为中国科学院。


Introduction

Analysis of Technical Requirements for Core Detection Elements


Neutral Atmosphere Detection Specifications

Satellites with an orbit altitude of 200-800km must be equipped with radio frequency plasma detectors, with key monitoring:

Parameter itemDetection rangeUncertainty
Atmospheric density1×10-16~1×10-10 kg/m³≤10%
Wind speed-1~1 km/s≤15 m/s

Comparison of ionospheric measurement indicators

Carrying a dual-frequency probe instrument in 1000-5000km orbit, key comparison parameters:

Element typeIon compositionDensity range
Conventional monitoringH⁺/He⁺1×10³~5×10¹² m⁻³
In-depth analysisO⁺ dominant layer±20% error limit

Technology evolution and implementation strategy

Compared with GJB2005, this standard adds the energy of radiation belt particle flux to 30MeV, and the detection accuracy of synchronous orbit electromagnetic field is improved to 0.3nT. It is recommended to use...

Typical application cases

  • Fengyun-4 geostationary orbit satellite uses three-level filtering to achieve DC electric field ≤1.0mV/m measurement accuracy
  • Beidou MEO constellation solves the problem of ion component identification through multi-probe matrix

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