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Modelling the interaction of micrometeoroid and technogenous particles with a space vehicle
- Authors: Syomkin N.D.1, Balakin V.L.1, Belokonov I.V.1, Voronov K.Y.1
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 6, No 1 (2007)
- Pages: 53-63
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/478
- DOI: https://doi.org/10.18287/2541-7533-2007-0-1(12)-53-63
- ID: 478
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Abstract
The number of particle collisions with a space vehicle (SV) is calculated on the basis of meteoric and technogenous environment. The space vehicle serves as a particle detector and is made in the form of a spherical inflatable filmy construction. The forecast of the number of collisions for the period of 2004-2012 is estimated. Dependences of the number of particles colliding with the SV are obtained as functions of its dimensions’ parameters and orbit parameters.
About the authors
N. D. Syomkin
Samara State Aerospace University
Author for correspondence.
Email: sadohina@ssau.ru
Russian Federation
V. L. Balakin
Samara State Aerospace University
Email: balakin@ssau.ru
Russian Federation
I. V. Belokonov
Samara State Aerospace University
Email: sadohina@ssau.ru
Russian Federation
K. Ye. Voronov
Samara State Aerospace University
Email: sadohina@ssau.ru
Russian Federation
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