Controlled separation of nanosatellites by means of the pulsed magnetic field
- Authors: Glushchenkov V.A.1, Yusupov R.Y.1
-
Affiliations:
- Samara University
- Issue: Vol 60, No 1 (2017)
- Pages: 1-8
- Section: Flight Vehicle Design
- URL: https://journal-vniispk.ru/1068-7998/article/view/229959
- DOI: https://doi.org/10.3103/S1068799817010019
- ID: 229959
Cite item
Abstract
A method of the controlled separation of nanosatellites from the carrier rocket by means of the pulsed magnetic field is described. Schemes of the separation device for group launch of satellites and results of exploratory experiments are given. A possibility of practical implementation of the method is considered.
About the authors
V. A. Glushchenkov
Samara University
Author for correspondence.
Email: vvz@ssau.ru
Russian Federation, shosse Moskovskoe 34, Samara, 443086
R. Yu. Yusupov
Samara University
Email: vvz@ssau.ru
Russian Federation, shosse Moskovskoe 34, Samara, 443086
Supplementary files
