Email this article Small-Size Automatic System for the Controllable Launch of Nanosatellites on a Desired Trajectory
- Authors: Filonin O.V.1, Belokonov I.V.1, Gimranov Z.I.1
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Affiliations:
- Samara University
- Issue: Vol 62, No 2 (2019)
- Pages: 184-191
- Section: Flight Vehicle Design
- URL: https://journals.rcsi.science/1068-7998/article/view/230907
- DOI: https://doi.org/10.3103/S1068799819020028
- ID: 230907
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Abstract
We consider the methods of mathematical modeling and calculation of main parameters of small-size magnetic induction ejectors (separation systems) for precision launch into orbit nano- and microsatellites. Examples of some technical solutions are presented.
About the authors
O. V. Filonin
Samara University
Email: zafargimranov86@gmail.com
Russian Federation, Moskovskoe shosse 34, Samara, 443086
I. V. Belokonov
Samara University
Email: zafargimranov86@gmail.com
Russian Federation, Moskovskoe shosse 34, Samara, 443086
Z. I. Gimranov
Samara University
Author for correspondence.
Email: zafargimranov86@gmail.com
Russian Federation, Moskovskoe shosse 34, Samara, 443086
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