# A Circularly Polarized HTS Microstrip Antenna Array with Controllable Cryostat

Authors: Xiaoyong Zeng; Kama Huang; Zhongxia Hu; Qian Chen; Wei Xiao
Journal: International Journal of Antennas and Propagation
 (2017)

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## Abstract

A high-temperature superconductor (HTS) microstrip antenna array with right-hand circular polarization is proposed for space communications. The proposed HTS antenna array can achieve high efficiency, which is able to reduce the antenna’s loss. The array consists of 16 antenna elements being fed by a T-network. A pair of symmetric meander slots is used in each antenna element to broaden the input matching bandwidth. A controllable cryostat is used as the refrigeration for HTS. The experiment shows that the gain of the proposed HTS antenna is 8.39 dB, whose 10 dB return loss bandwidth is 2.2% ranging from 5.75 GHz to 5.87 GHz. In comparison with a traditional conductor antenna array having the same configuration, the proposed array has an 8.1 dB improvement in the gain and a 69.2% enhancement in the radiation efficiency.


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## Body

## 1. Introduction

Antenna is an important component for space communication, where some characteristics of the antennas are highly desired, including high gain, high efficiency, low profile, and low cost [1]. The microstrip antenna array having the advantages of high gain and low profile and the convenience of fabrication is considered as a good candidate [2, 3]. However, due to the conductor loss, the microstrip antenna suffers from relatively low efficiency, especially in antenna arrays with feed networks [3].In order to overcome this defect, the high-temperature superconductor (HTS) with low conductor loss has been used in antennas for high efficiency [4–11]. The use of the HTS in the antenna can lead to the reduction of the loss of the matching circuit and feed network, which is proportional to the conductor loss [2, 3]. Besides, the HTS is able to suppress the undesirable surface-wave of the antenna, thus increasing the radiation efficiency [4]. For example, the work [5] proposed a miniaturized HTS microstrip patch antenna, which achieved the good radiation efficiency between 35% and 65%. In [6], a HTS helical antenna was designed, and its efficiency is 70%. Reference [7] proposed a HTS antenna array with a measured gain of 1.54 dB.Usually, the working temperature of the HTS is about 80 K, and thus a cryostat should be created for the HTS antenna. In traditional designs [4–11], liquid nitrogen is used for the cryostat. Yet, the liquid nitrogen should be refreshed continuously for stable temperature, so it is hard to control the temperature accurately. Different from the liquid nitrogen, a new commercial Stirling refrigerator has the ability to accurately control the temperature from 60 K to 300 K by computers, which is more suitable and affordable as the cryostat for the HTS antenna.In this paper, a HTS microstrip antenna array with right-hand circular polarization is designed at 5.8 GHz. It is fabricated withDyBCO on a LaAlO3 substrate by thermal coevaporation. The array is comprised of 16 antenna elements being fed by a T-network. In the antenna, two truncated corners are used to generate the circular polarization, and a pair of symmetric meander slots is used to broaden the input matching bandwidth. A Stirling refrigerator is employed as the controllable cryostat. Compared with a traditional conductor antenna with the same configuration, the HTS antenna array has high radiation efficiency.


## 2. Design of the HTS Antenna Array

### 2.1. Design of the Antenna Element

Figure1 depicts the configuration of the HTS antenna array’s element, which is a square microstrip antenna. Two truncated corners and a pair of symmetric slots are etched for the circular polarization and broad input matching bandwidth, respectively. The substrate is made of LaAlO3 having a thickness of 0.5 mm with the relative permittivity of 24.Figure 1
The configuration of the HTS antenna array’s element.According to [2], the square patch will create a resonance, whose frequency f1 can be calculated by (1)f1=c2Ls1+εr,where c is the speed of the light in free space, Ls is side-length of the square, and εr is the relative permittivity of the substrate. With the truncated corners, another orthogonal resonance will be created [7]. Correspondingly, the resonance frequency f2 can be expressed as(2)f2=f11-Lc2Ls2,where Ls2 is the area of the square patch and Lc2 is the area of the two truncated corners. f1 and f2 are set to close properly, and hence the frequency band between them can be with the circular polarization.Due to the high permittivity and thin thickness of the substrate, a high quality factor of the antenna is obtained. Thus the input matching bandwidth is narrow, only ranging from 0.85% to 1.1% [11]. In order to improve the bandwidth of the antenna, a pair of symmetric meander slots is etched on the patch, and hence two new resonance modes TM20 and TM30 are created [12]. With the proper dimension of slots, the frequency of TM20 and TM30 is adjacent, so the input matching bandwidth can be broadened. Besides, ds and gs are the length and width of the slot, respectively, which are obtained by sweeping parameters with the CST Microwave Studio, a popular full-wave simulator. The feed line for the antenna is with an impedance of 100 Ω and Wl is the width of the feed line. The optimized parameters values are listed in Table 1.Table 1
Parameters of the antenna element.
Parameter
Value (mm)
L
s
5.27
L
c
0.59
D
s
1.80
G
s
0.18
W
l
0.17


### 2.2. Design of the Antenna Array

The configuration of the HTS antenna array is shown in Figure2, which consists of 16 antenna elements designed in the previous section. The array is fed by a three-level T-network with quarter-wave impedance transformers. As shown in Figure 2, the impedance of the feed line for antenna elements is 100 Ω, and the shunt impedance of two feed lines is 50 Ω. Hence, the transformer’s impedance is set to 70 Ω [13].Figure 2
The configuration of the HTS antenna array.The parametersdx and dz are the separated distances between antenna elements along x- and z-axes. With consideration of the mutual coupling between antenna elements and dimension of the array, dx and dz are set to 17.5 mm, and the size of the array is 69mm∗72.25mm. Using CST, the HTS antenna array is simulated. The directivity and gain of the antenna at 5.8 GHz are 11.54 dBi and 10.87 dB, respectively. The radiation efficiency reaches 85.7%.


### 2.3. Controllable Cryostat for the HTS Antenna Array

Figure3 shows the configuration of the cryostat for the HTS antenna array. The main components of the cryostat are a Stirling refrigerator and a stainless-steel cavity. The Stirling refrigerator is used to control the temperature with a computer, while the airtight stainless-steel cavity is used to provide a vacuum for low temperature. The antenna is placed on a supporting tray in the cavity, and a radome with the relative permittivity of 4 is employed as a superstrate for sealing. The cryostat is simple and compact, and thus it is perfect for the HTS antennas.Figure 3
The configuration of the controllable cryostat for the HTS antenna.


## 2.1. Design of the Antenna Element

Figure1 depicts the configuration of the HTS antenna array’s element, which is a square microstrip antenna. Two truncated corners and a pair of symmetric slots are etched for the circular polarization and broad input matching bandwidth, respectively. The substrate is made of LaAlO3 having a thickness of 0.5 mm with the relative permittivity of 24.Figure 1
The configuration of the HTS antenna array’s element.According to [2], the square patch will create a resonance, whose frequency f1 can be calculated by (1)f1=c2Ls1+εr,where c is the speed of the light in free space, Ls is side-length of the square, and εr is the relative permittivity of the substrate. With the truncated corners, another orthogonal resonance will be created [7]. Correspondingly, the resonance frequency f2 can be expressed as(2)f2=f11-Lc2Ls2,where Ls2 is the area of the square patch and Lc2 is the area of the two truncated corners. f1 and f2 are set to close properly, and hence the frequency band between them can be with the circular polarization.Due to the high permittivity and thin thickness of the substrate, a high quality factor of the antenna is obtained. Thus the input matching bandwidth is narrow, only ranging from 0.85% to 1.1% [11]. In order to improve the bandwidth of the antenna, a pair of symmetric meander slots is etched on the patch, and hence two new resonance modes TM20 and TM30 are created [12]. With the proper dimension of slots, the frequency of TM20 and TM30 is adjacent, so the input matching bandwidth can be broadened. Besides, ds and gs are the length and width of the slot, respectively, which are obtained by sweeping parameters with the CST Microwave Studio, a popular full-wave simulator. The feed line for the antenna is with an impedance of 100 Ω and Wl is the width of the feed line. The optimized parameters values are listed in Table 1.Table 1
Parameters of the antenna element.
Parameter
Value (mm)
L
s
5.27
L
c
0.59
D
s
1.80
G
s
0.18
W
l
0.17


## 2.2. Design of the Antenna Array

The configuration of the HTS antenna array is shown in Figure2, which consists of 16 antenna elements designed in the previous section. The array is fed by a three-level T-network with quarter-wave impedance transformers. As shown in Figure 2, the impedance of the feed line for antenna elements is 100 Ω, and the shunt impedance of two feed lines is 50 Ω. Hence, the transformer’s impedance is set to 70 Ω [13].Figure 2
The configuration of the HTS antenna array.The parametersdx and dz are the separated distances between antenna elements along x- and z-axes. With consideration of the mutual coupling between antenna elements and dimension of the array, dx and dz are set to 17.5 mm, and the size of the array is 69mm∗72.25mm. Using CST, the HTS antenna array is simulated. The directivity and gain of the antenna at 5.8 GHz are 11.54 dBi and 10.87 dB, respectively. The radiation efficiency reaches 85.7%.


## 2.3. Controllable Cryostat for the HTS Antenna Array

Figure3 shows the configuration of the cryostat for the HTS antenna array. The main components of the cryostat are a Stirling refrigerator and a stainless-steel cavity. The Stirling refrigerator is used to control the temperature with a computer, while the airtight stainless-steel cavity is used to provide a vacuum for low temperature. The antenna is placed on a supporting tray in the cavity, and a radome with the relative permittivity of 4 is employed as a superstrate for sealing. The cryostat is simple and compact, and thus it is perfect for the HTS antennas.Figure 3
The configuration of the controllable cryostat for the HTS antenna.


## 3. Measurement and Antenna Performance

The designed HTS antenna array is fabricated as shown in Figure4(a). Figure 4(b) displays the photograph of the cryostat. The input reflection coefficient S11 of the HTS antenna array at the temperature of 80 K is measured by an Agilent E8362B Vector Network Analyzer. In Figure 5, the measured and simulated input reflection coefficients agree well with each other. The measured reflection coefficient is −15 dB at the working frequency of 5.8 GHz and the 10 dB return loss bandwidth is 2.2% ranging from 5.75 GHz to 5.88 GHz.Figure 4
The photograph of the fabricated (a) HTS antenna array and (b) cryostat.
(a)
(b)Figure 5
The simulated and measured input reflection coefficients of the HTS antenna array.The radiation performance of the HTS antenna array is measured by a NSI system in the anechoic chamber. The radiation patterns and axial ratio of the HTS antenna array at the frequency of 5.8 GHZ and the temperature of 80 K are shown in Figures6 and 7, respectively. The beamwidths of the HTS antenna array on X and Z planes are 27° and 30°, respectively, while the simulated beamwidths are 23.7° and 28°. The axial ratio is lower than 4 at broadside.Figure 6
The simulated and measured radiation patterns of the HTS antenna array at the frequency of 5.8 GHz and the temperature of 80 K on (a)X and (b) Z planes.
(a)
(b)Figure 7
The simulated and measured axial ratio of the HTS antenna array at the frequency of 5.8 GHz and the temperature of 80 K on (a)X and (b) Z planes.
(a)
(b)Moreover, the circularly polarized gain of the HTS antenna array is obtained by(3)G=10lg⁡10GH/10+10GV/10,where GH and GV are the measured gain of the antenna on the horizontal and perpendicular planes, respectively. Figure 8 gives the gains of the HTS antenna array at 5.8 GHz against the temperature from 60 K to 90 K. It is observed that the gain is a constant of 8.39 dB below the temperature of 83 K. While the temperature exceeds 83 K, the gain decreases dramatically.Figure 8
The measured gain of the HTS antenna array at the frequency of 5.8 GHz against the temperature from 60 K to 90 K.Furthermore, a traditional conductor antenna array with the same configuration of the HTS one is simulated, fabricated and measured for comparisons. The simulated directivity and gain at 5.8 GHz are 9.92 dBi and 2.10 dB, respectively. The radiation efficiency is 16.5%. Figure9 shows the radiation patterns of the traditional conductor antenna array. The measured gain is 0.32 dB. In comparison with the traditional antenna array, the proposed array has an 8.07 dB improvement in the gain and a 69.2% enhancement in the radiation efficiency.Figure 9
The simulated and measured radiation patterns of the traditional conductor antenna array at the frequency of 5.8 GHz on (a)X and (b) Z planes.
(a)
(b)


## 4. Conclusion

In this paper, a HTS microstrip antenna array with right-hand circular polarization is designed for space communication. A controllable cryostat is used for the HTS antenna. Using meander slots, a broad bandwidth of the antenna is obtained. The HTS antenna array’s gain and radiation efficiency are 8.39 dB and 85.7%, respectively. In comparison with a traditional conductor antenna array having the same configuration, 8.1 dB and 69.2% improvements in antenna gain and radiation efficiency are achieved, respectively. The HTS antenna array shows more excellent performances than the traditional one, which has the potential in the space communication.



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*Source: 6035202-2017-07-20.xml*