Computer simulation of spacecraft/environment interaction.

K K Krupnikov; A A Makletsov; V N Mileev; L S Novikov; V V Sinolits

doi:10.1016/s1350-4487(99)00225-5

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Computer simulation of spacecraft/environment interaction.

K K Krupnikov·A A Makletsov·V N Mileev·L S Novikov·V V Sinolits

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Abstract

This report presents some examples of a computer simulation of spacecraft interaction with space environment. We analysed a set data on electron and ion fluxes measured in 1991 1994 on geostationary satellite GORIZONT-35. The influence of spacecraft eclipse and device eclipse by solar-cell panel on spacecraft charging was investigated. A simple method was developed for an estimation of spacecraft potentials in LEO. Effects of various particle flux impact and spacecraft orientation are discussed. A computer engineering model for a calculation of space radiation is presented. This model is used as a client/server model with WWW interface, including spacecraft model description and results representation based on the virtual reality markup language.

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Computer Simulation Cosmic Radiation Extraterrestrial Environment Internet Ions Models, Theoretical Protons Radiation Dosage Radiation Monitoring Software Solar Activity Space Flight Spacecraft Journal Article

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K K Krupnikov, A A Makletsov, V N Mileev, L S Novikov, V V Sinolits. 1999. Computer simulation of spacecraft/environment interaction.. https://doi.org/10.1016/s1350-4487(99)00225-5

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