PIERS Proceedings, Marrakesh, MOROCCO, March 20–23, 2011 458 The Application in Spacecraft of High Temperature Superconducting Magnetic Energy Storage Bo Yi1 and Hui Huang1, 2 1 School of Electrical Engineering, Beijing Jiaotong University, Beijing 100044, China 2 State Key Laboratory of Millimeter Waves, Nanjing 210096, China Abstract— This paper has analyzed the requirement of energy storage devices in spacecraft and introduced the present development situation of high temperature superconducting magnetic energy storage technology, then conceives an idea that applying the skill of high temperature superconducting magnetic energy storage in spacecraft to replace the existing energy storage devices in spacecraft. Also, a comprehensive comparing among the high temperature superconducting magnetic energy storage technology and other existing energy storage technologies such as flywheel energy storage technology, battery energy storage technology has been done. The conclusion that the high temperature superconducting magnetic energy storage technology has more advantages than other existing energy storage technologies in application of aerospace technology is reached. 1. THE REQUIREMENT OF ENERGY STORAGE DEVICES IN SPACECRAFT Energy storage devices in spacecraft is used for transforming chemical energy and other types of energy into electric energy. Its main functions are below: (1) supplying electricity from spacecraft being launched to the time that solar panels started; (2) supplying electricity for spacecraft at dark period; (3) supplying auxiliary electricity when the supplying of solar battery is not sufficient at light period. Spacecrafts usually adopt battery as energy storage devices. But there are many obvious deficiencies, which will be mentioned below. Since the performance and lifetime of energy storage devices have limited the development of spacecraft for a long time, spacecraft has such aspects of requirements for energy storage devices: (1) the requirements for electrical property such as high energy, small mass and high power; (2) properly sealed in case of electrolyte evaporation for chemical battery; (3) capable of resisting for mechanical environments; (4) the requirements for heat output [1]. 2. THE PRESENT DEVELOPMENT SITUATION OF HIGH TEMPERATURE SUPERCONDUCTING MAGNETIC ENERGY STORAGE TECHNOLOGY Superconducting magnetic energy storage (SMES) is a remarkable application of superconducting magnets, especially for high temperature superconducting magnetic energy storage technology (HTSMES). The potential utilization of high-temperature superconducting materials is especially promising in order to obtain energy storage devices showing high efficiency and lifetime HTSMES device is made up of a superconducting coil, a power conditioning system and a refrigerator and a vacuum to keep the coil at low temperature. It stores electric energy as direct electric current passing through a superconducting coil. Because the superconducting material has nearly zero resistance, the electric current can almost circulate indefinitely. The energy stored in the coil can be calculated by the formula E = 0.5LI 2 , where L is the inductance of the coil and I is the current passing through it. Storage capacity for HTSMES is quite outstanding. For SMES, it can be anything up to 20 MW. SMES devices can run for thousands of charge/discharge cycles without any degradation to the magnet, giving it a life of 20+ years. In the recent study, some scientists proposed the design of 300 MJ I-ITS superconducting magnetic energy storage system. In addition, from 2004 to 2007, a 10 MVA/20 MJ SMES prototype for a 100 MW commercial system was developed in Japan [2]. In 2010, the superconducting magnet designed with the basic requirements including a total storage energy of 2 MJ and a storage energy density of 2.73 MJ/m3 has been achieved [3]. 3. APPLYING THE SKILL OF HIGH TEMPERATURE SUPERCONDUCTING MAGNETIC ENERGY STORAGE IN SPACECRAFT Due to the lack of air convection when spacecraft is on the orbit, the temperature of the side face to Sun can be heated to above 373 K while the temperature of the other side can be below 173 K. Progress In Electromagnetics Research Symposium Proceedings, Marrakesh, Morocco, Mar. 20–23, 2011 459 The extreme temperature difference makes a perfect environment for applying of superconducting. In addition, although it costs a lot and takes a large proportion of volume and mass for a refrigerator and a vacuum to keep the coil at low temperature at superconducting storage devices, the refrigerator and devices to keep vacuum are not needed in space any more, which also makes the applying of HTS-SMES in spacecraft has more advantages. However, the biggest problem for applying HTSMES in to spacecraft is the relatively low energy density, which is expected to solve in the inherent low temperature environment like in space. 4. A COMPREHENSIVE COMPARING AMONG THE HIGH TEMPERATURE SUPERCONDUCTING MAGNETIC ENERGY STORAGE TECHNOLOGY AND OTHER EXISTING ENERGY STORAGE TECHNOLOGIES (1) Storage battery Storage battery has such deficiencies: (1) the scope of its temperature admission is narrow; (2) the discharge capacity and efficiency decreased as the increasing of the number of recharge cycles; (3) the lifetime is short; (4) it takes much time for charging; (5) it may cause pollution. (2) Flywheel energy storage A flywheel is a mechanical device with a significant moment of inertia used as a storage device for rotational energy. The flywheel is proving to be an ideal form of energy storage on account of its high efficiency, long cycle life, wide operating temperature range, freedom from depth-of-discharge effects, and higher power and energy density — on both a mass and a volume basis [4–6]. There also some scientists proposed that the application of flywheel on satellite energy storage/attitude control system (ACS), which has advantages shown in Table 1 below [7]. Table 1: The advantages of ACS. the characteristic of attitude control system long lifetime large moment of control force high efficiency high energy density advantages decrease the cost of maintaining and replacing energy storage decrease the requirement of propulsion force decrease the cost of energy decrease the mass of energy storage devices But when the ACS is operating, it can be a big disturb to the attitude of spacecraft, which will affect the normal operation of spacecraft. This is a very complicated nonlinear system, whose control is very difficult to achieve, especially for spacecraft with small mass. (3) High temperature superconducting magnetic energy storage HTSMES systems have the following advantages compared to other energy storage systems: 1. High cyclic efficiency — HTSMES can achieve an high overall cyclic efficiency; 2. Fast response time — HTSMES has pure electrical energy conversion, whilst other energy storage devices involve either electrical-chemical or electrical-mechanical energy conversion, which is much slower; 3. Deep discharge and recharge ability — unlike batteries, HTSMES can discharge and recharge fully for an unlimited number of times; 4. Good balance between power density and energy density — although SMES does not have the highest power density or the highest energy density, it does have a good balance between them, which is very important for aircraft systems [8]. 5. CONCLUSION As technology develops, the energy density of HTSMES can be enhanced especially for application in space environment. Compared to HTSMES, then traditional battery storage has obvious disadvantages and has no special advantages. For flywheel energy storage, its obvious advantage is that the operation of flywheel is a big disturb for the stability of spacecraft, which may make the control of the whole spacecraft too complicated. What’s more, the future trend for flywheel energy storage is also adopting superconducting to increase its efficiency, which makes flywheel energy storage have the same parts of device used for keeping its soil in low temperature as the 460 PIERS Proceedings, Marrakesh, MOROCCO, March 20–23, 2011 HTSMES. On the contrary, HTSMES will not bring about a disturb. Although its energy density may be lower than flywheel storage now, its energy density will increased because there is no need for refrigerator in space And in order to ensure its operation environment, we can at least adopt hybrid system including battery and HTSMES or ACS and HTSMES, which may alleviate the disturb to an extent that can be controlled and satisfy the energy supply at the same time. REFERENCES 1. Li, G. 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