ISO 14200 specifies a common process for selecting and implementing meteoroid and space debris environment models used in the impact flux assessment for the design and operation of spacecraft and other purposes.
Meteoroid and space debris environment models can be used to estimate the impact fluxes of meteoroids and space debris on a spacecraft. This flux information can be used in:
ISO 14200 provides guidelines and requirements for the process.
ISO 14200 on meteoroid and space debris environment models is applicable for:
Every spacecraft in an Earth orbit is exposed to a certain flux of micrometeoroids and man-made space debris. Collisions with these particles take place with hypervelocity. Meteoroid and space debris environment models have been developed which describe populations of meteoroids and/or space debris.
ISO 14200 provides you with common implementation process for meteoroid and space debris environment models, which is used for estimation of the impact flux required when selecting the spacecraft operation orbit, evaluation of the impact flux in a specific orbit, prediction of the frequency of collision avoidance operations, and estimate of the impact flux required for protection design.
Following guidelines provided in ISO 14200, you can protect space stations from meteoroid and space debris.
ISO 14200 describes procedures that are available to guide a user in the selection and implementation of a suitable model. To select a suitable environment model, the capabilities of available candidate models should be considered.
BS ISO 14200:2021 supersedes BS ISO 14200:2012. BS ISO 14200:2021 includes some technical changes concerning BS ISO 14200:2012. These include:
ISO 14200