Superconducting Magnetic Energy Storage and Superconducting Self-Supplied Electromagnetic Launcher★

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Superconducting Magnetic Energy Storage and Superconducting Self-Supplied Electromagnetic Launcher★ Eur. Phys. J. Appl. Phys. 80, 20901 (2017) THE EUROPEAN © EDP Sciences, 2017 PHYSICAL JOURNAL DOI: 10.1051/epjap/2017160452 APPLIED PHYSICS Regular Article Superconducting magnetic energy storage and superconducting self-supplied electromagnetic launcher★ Jérémie Ciceron*, Arnaud Badel, and Pascal Tixador Institut Néel, G2ELab CNRS/Université Grenoble Alpes, Grenoble, France Received: 5 December 2016 / Received in final form: 8 April 2017 / Accepted: 16 August 2017 Abstract. Superconductors can be used to build energy storage systems called Superconducting Magnetic Energy Storage (SMES), which are promising as inductive pulse power source and suitable for powering electromagnetic launchers. The second generation of high critical temperature superconductors is called coated conductors or REBCO (Rare Earth Barium Copper Oxide) tapes. Their current carrying capability in high magnetic field and their thermal stability are expanding the SMES application field. The BOSSE (Bobine Supraconductrice pour le Stockage d’Energie) project aims to develop and to master the use of these superconducting tapes through two prototypes. The first one is a SMES with high energy density. Thanks to the performances of REBCO tapes, the volume energy and specific energy of existing SMES systems can be surpassed. A study has been undertaken to make the best use of the REBCO tapes and to determine the most adapted topology in order to reach our objective, which is to beat the world record of mass energy density for a superconducting coil. This objective is conflicting with the classical strategies of superconducting coil protection. A different protection approach is proposed. The second prototype of the BOSSE project is a small-scale demonstrator of a Superconducting Self-Supplied Electromagnetic Launcher (S3EL), in which a SMES is integrated around the launcher which benefits from the generated magnetic field to increase the thrust applied to the projectile. The S3EL principle and its design are presented. 1 Motivation supply of an electromagnetic launcher, or through a voltage adaptation system if the discharge has to be controlled. 1.1 SMES principle [1] SMES have low energy density compared to batteries, but high power densities. Furthermore, they can have high Superconductors have the property to lose their electrical cycling yield (97%), with the cycling yield being defined as resistivity when they are cooled under a critical temperature the recovered energy divided by the energy provided to the TC. Even if energy dissipation occurs in a superconductor SMES, including the energy spent to cool the system, after submitted to variable electrical current or magnetic induc- one cycle. They are direct electricity storage devices such as tion (B), there is no energy dissipation in a steady state. If a capacitors. Nevertheless, they can have much higher superconducting winding is supplied, then short-circuited energy density than high power capacitor banks. The current is not dissipated by Joule effect and magnetic energy volume energy of a SMES can be roughly estimated if the B is conserved almost indefinitely. This is the principle of field is considered homogeneous in the SMES and if the inductive storage with superconductors, generally called winding thickness is neglected. In these conditions, SMES (Superconducting Magnetic Energy Storage). equation (1) gives a volume energy of 32 MJ/m3 for a 3 The stored energy Emag can be expressed as a function of SMES having a homogeneous field of 9 T, and 57 MJ/m for inductance L and current I or as the integral over space of the 12 T. In comparison, the volume energy of high power product of magnetic field H by induction B, following (1): capacitor banks is around 1 MJ/m3. Thanks to High fi 1 1 Temperature Superconductors (HTS), a SMES with a eld ¼ 2 ¼ ∭ : ð1Þ of 12 T or even more is feasible. Second generation HTS Emag 2 LI 2 BHdx dy dz Space conductors, also called coated conductors or REBCO (Rare Earth, Barium, Copper Oxide) tapes, are the most Once the SMES has been charged and short-circuited, performing superconductors today in terms of critical the energy is available and can be used by opening the short temperature as well as in terms of engineering current circuit and connecting the SMES to a load. It can be under high magnetic fields. They offer the opportunity to connected to the load either directly as in the case of direct largely improve the performances of SMES in terms of mass, volume, thermal stability and therefore to expand ★ fi Contribution to the topical issue “Electrical Engineering their application eld. Even if the critical temperature of Symposium (SGE 2016)”, edited by Adel Razek these tapes is high (90 K), they are generally used at 4.2 K * e-mail: [email protected] (liquid helium bath) in high field applications because the 20901-p1 2 J. Ciceron et al.: Eur. Phys. J. Appl. Phys. 80, 20901 (2017) Fig. 1. Schematic layout of REBCO tapes. The layers are not up to scale (courtesy C. Barth, University of Geneva). F projectile I rail B B I I B Fig. 2. Principle diagram of an electromagnetic launcher (railgun) and picture of the PEGASUS launcher (10 MJ). more a superconductor is cooled, the more its current an electrical current of 1 MA [6]. Electromagnetic launch- carrying capability is increased. On the contrary, the ers are generally supplied by capacitor banks. These are higher is the B field, the lower is the current carrying very voluminous because of their low energy density on one capability. REBCO conductors are commercially available side, and because of the poor supply chain yield on the in the form of flat tapes (see Fig. 1) which are commonly other side. A SMES, being an inductive pulse power source, around 100 mm thick; custom thicknesses are availed from is particularly adapted for supplying directly an electro- some manufacturers. magnetic launcher with rails [7]. Combination of modest energy density with very high In mostofthelaunchers(i.e.PEGASUS),theinductionB power density naturally leads to consider SMES as pulse is only generated by the current passing in the rails. But it is current source or connected to the grid to compensate short possible to increase the value of B between the rails thanks to power faults [2]. additional windings, parallel to the rails, and then to increase the propulsive thrust applied to the projectile. In this case, 1.2 Intended application the term “augmented launcher” is used. The S3EL (Superconducting Self-Supplied Electromag- Since 2004, a program for the development of SMES has netic Launcher) concept [8] is combining a powering by been led at Grenoble CNRS [3] in order to consider HTS SMES with the augmented launcher principle. The energy SMES as power source to supply electromagnetic launch- which is required for the launch is stored in racetrack-shaped ers. An electromagnetic launcher, commonly called “rail- windings surrounding the rails and then is released in these gun”, is made of two parallel conductive rails, with a last ones. The magnetic induction generated by the windings projectile establishing a sliding contact between them. A is increasing the propelling thrust and the projectile output high electrical current passing through the rails and the velocity. Otherwise, it can reduce the current required to projectile is accelerating the projectile, according to the reacha givenoutputvelocity.Intheend,thisconceptenables same principle as in the famous Laplace rail experiment. to lighten and to compact the launcher supply chain. The force applied to the projectile is: Furthermore, the windings being magnetically coupled to the rails, a part of rails magnetisation energy is recovered by F~ ¼ I~ℓ Â B~; ð2Þ the superconducting windings at the end of the shot, improving the launch global yield and reducing the energy where ℓ is the distance between rails, I is the current dissipated in the muzzle electric arc which happens when the passing in the projectile and B is the magnetic induction on projectile is leaving the rails. the projectile. Nevertheless, to make such a device at full scale is These launchers (see Fig. 2) can propel projectiles at technologically very challenging because a launcher higher velocities than conventional powder guns and nominal current is in the range of several tens or hundreds research is ongoing in several countries on this topic of kA, and can even be several MA for large size launchers. [4,5]. In the 10 MJ PEGASUS launcher developed at ISL, Even if cables with currents of several kA have been the projectile can reach an output velocity of 2000 m/s for manufactured and tested under field [9,10], cables with 20901-p2 J. Ciceron et al.: Eur. Phys. J. Appl. Phys. 80, 20901 (2017) 3 currents in the range of hundreds of kA or more are not solutions, a solenoid and a torus, have been studied in existing today. Another solution consists in using the detail. Their performances are finally rather close and both SMES as a buffer power supply in order to quickly recharge solutions have advantages and drawbacks. a capacitor bank. In this case, the capacitor bank is sized only for one shot [11] but the launcher can fire in bursts. 2.2 Considerations about magnetic energy storage The objective of the BOSSE project of French 2.2.1 Virial theorem Directorate General of Armaments (DGA) is to develop the technology of HTS magnets with very high energy The torus has the advantage of a minimal stray field. The density, foreseeing what could be a buffer energy storage solenoid is minimizing the required amount of conductor in for large size launchers, and to test at low scale the case of an isotropic conductor as well as the amount of feasibility of a coupled S3EL launcher. This will be associated structural material.
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