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| Content Provider | IEEE Xplore Digital Library |
|---|---|
| Author | Reck, B. |
| Copyright Year | 1965 |
| Abstract | The principle of electromagnetic launch remains a permanent subject of military research because of its outstanding advantages. For instance, the acceleration profile is completely under control. The railgun is the first choice to accelerate low masses from some grams to several kilograms up to velocities greater than 1000 m/s. On the contrary, accelerating heavy masses such as combat aircraft leads to quite different solutions, namely to the use of linear induction machines. We have studied the launch of an unmanned air vehicle (UAV) weighing several hundred kilograms up to an initial velocity of 50 m/s with a linear synchronous motor (LSM) capable of replacing chemical boosters or mechanical launchers. This paper presents a basic concept study of a catapult for launching a UAV by means of an LSM. A numerical code has been developed to give the main characteristics (thrust, input power, efficiency, current, mass) of the launch system. |
| Sponsorship | IEEE Magnetics Society |
| Starting Page | 310 |
| Ending Page | 313 |
| Page Count | 4 |
| File Size | 235987 |
| File Format | |
| ISSN | 00189464 |
| Volume Number | 39 |
| Issue Number | 1 |
| Language | English |
| Publisher | Institute of Electrical and Electronics Engineers, Inc. (IEEE) |
| Publisher Date | 2003-01-01 |
| Publisher Place | U.S.A. |
| Access Restriction | One Nation One Subscription (ONOS) |
| Rights Holder | Institute of Electrical and Electronics Engineers, Inc. (IEEE) |
| Subject Keyword | Unmanned aerial vehicles Acceleration Synchronous motors Chemicals Rails Gravity Electromagnetic launching Railguns Aircraft Mechanical variables control |
| Content Type | Text |
| Resource Type | Article |
| Subject | Electronic, Optical and Magnetic Materials Electrical and Electronic Engineering |
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