Design of an Electromagnetic Launcher for Earth-to-Orbit (ETO) Microsatellite Systems

被引：1

作者：

Hasirci, Ugur ^{[1
]}

Balikci, Abdulkadir ^{[1
]}

机构：

[1] Gebze Inst Technol, Dept Elect Engn, Kocaeli, Turkey

来源：

RAST 2009: PROCEEDINGS OF THE 4TH INTERNATIONAL CONFERENCE ON RECENT ADVANCES IN SPACE TECHNOLOGIES | 2009年

关键词：

electromagnetic launchers; coilguns; railguns; microsatellite systems; LINEAR INDUCTION LAUNCHERS; SPACE APPLICATIONS; PERFORMANCE; GUN; COILGUNS;

D O I：

10.1109/RAST.2009.5158203

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

In this study, an alternative launcher design for Earth-to-Orbit (ETO) microsatellite systems is addressed. The main goal of the design is to reduce the cost of launching operation. For this aim, a new topology is introduced and a sample design is presented. The paper proposes a vertical takeoff Electromagnetic Launcher (EML) for ETO microsatellite systems. Design specifications are 6 km/s muzzle velocity and 20000 Gee's acceleration for a 100 kg payload. It is expected that proposed design presents a powerful alternative to conventional launchers and existing electromagnetic launchers for ETO systems.

引用

页码：233 / 236

页数：4

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