Controlled separation of nanosatellites by means of the pulsed magnetic field

被引：0

作者：

Glushchenkov V.A. ^{[1
]}

Yusupov R.Y. ^{[1
]}

机构：

[1] Samara University, shosse Moskovskoe 34, Samara

来源：

Glushchenkov, V.A. (vvz@ssau.ru) | 2017年 / Allerton Press Incorporation卷 / 60期

关键词：

capacitive energy storage; inductor; nanosatelite; pulsed magnetic field;

D O I：

10.3103/S1068799817010019

中图分类号：

学科分类号：

摘要：

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. © 2017, Allerton Press, Inc.

引用

页码：1 / 8

页数：7

共 7 条

[1]

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[2]

Sarokvasha P.Y., Shulepov A.I., Tarasov Y.L., Arrangement of a Spacecraft-Borne Scientific Instrument Container in the Passing Experiment, Izv. Vuz. Av. Tekhnika, 52, 1, pp. 11-14, (2009)

[3]

ISIS [Electronic resource]

[4]

Glushchenkov V.A., Yusupov R.Y., Belokonov I.V., Gimranov Z.I., RU Patent 2472679, Byul. Izobr., (2013)

[5]

Kim K.K., Use of Electrodynamic Accelerometers for Aviation and Space Purposes, Izv. Vuz. Av. Tekhnika, 46, 1, pp. 27-30, (2003)

[6]

Belokonov I.V., Filonin O.V., Talyzin Y.B., RU Patent 2551408, Byul. Izobr., (2015)

[7]

Yusupov R.Y., Glushchenkov V.A., Belokonov I.V., Gimranov Z.I., RU Utility Model Patent 140953, Byul. Izobr., (2014)

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