Abstract

We propose a novel, compact, prime-focus antenna feed for space communication. The feed requires full-wave simulator optimization for a given parabolic reflector and is designed to operate simultaneously on two bands, offering LHC/RHC polarizations for the 13 cm band and V/H polarizations for the 70 cm band. With performance results confirmed by measurement, it has been verified in practice that this compact feed is suitable for use in a low-noise Earth-Moon-Earth communication link.

1. Introduction

Amateur radio Moon Bounce, EME (Earth-Moon-Earth), communication is a very technically demanding discipline [1]. Usually, high-gain reflector antennas are used, but they require appropriate prime-focus feeds designed mainly for low-noise operation [1].

EME communications do not require simultaneous multiband operation; so, to change the working band, a station operator has enough time to exchange prime-focus feeds.

Additionally, the antenna gain depends on the diameter of the dish reflector, which is very often limited by space and operating cost requirements. For users, it is very important to squeeze every possible tenth of a dB from their antennas, recognizing the inherent lack of adequate gain. This requirement is in contrast to the effectiveness of multiband reflector antennas whose efficiency is usually lower than that of monoband antennas due to the compromised designs of their feeds.

Dual-band or multiband prime-focus feeds are used only by stations equipped with electrically large and especially physically large-size reflectors, where replacement of the prime feed is mechanically very demanding, expensive, or difficult to implement.

A description of a 10 m dish antenna’s dual-band primary feed for the 70/23 cm bands was published by Doug McArthur [2]. McArthur’s feed consisted of a dual-mode waveguide feed for 23 cm surrounded by four dipoles for 70 cm. See Figure 1.

Since the dipoles’ impedance is about 105 ohms, they must be impedance-matched by employing feed lines of λ/4 length with 72.5 ohm impedance. This design also requires isolating the dipoles from their ground plane, see Figure 2.

This solution introduces unwanted and unpredictable impedance behavior, especially when the feed is mounted onto a dish. However this design was successfully fabricated by several operators worldwide [2]. Unfortunately, measured radiation patterns were not disclosed by the author. Similar solution consisting of waveguide and dipoles has been recently reported for X/Ka bands [3].

The proposed design of a dual-band prime-focus feed utilizing butterfly-shaped dipoles and a ground plane subreflector equipped with a choke can be regarded as a completely novel approach for coverage of EME 70/13 cm bands.

This paper describes a compact, dual-band feed (70/13 cm–432/2320 MHz) intended for a parabolic reflector with a diameter of 6.4 m and f/D ratio of 0.4. Horizontal and vertical polarizations are available on the 432 MHz band. The 2320 MHz band feed can operate with both right and left-hand circular polarization. Hence, this compact feed offers dual polarization operation at both bands.

2. Requirements for Dual-Band Prime-Focus Feed

Above considerations dictate the following requirements for the dual-band feed: (1)high gain in antenna assembly—minimal blockage of reflector;(2)low noise—edge taper about 15 dB;(3)low backward radiation; (4)RHC- and LHC-polarization capability with good axial ratio for 2320 MHz (13 cm band);(5)vertical and horizontal polarization for 432 MHz (70 cm) band;(6)able to handle high power, up to 3 kW with very good impedance match;(7)low weight <7 Kg (in order to avoid mechanically distorting the shape of the parabolic reflector).

It should be emphasized that the feed needs not to be broadband since, for the EME purposes, the following frequencies are used: 432.050 MHz ± 50 kHz on 70 cm and two frequencies 2304.050 MHz ± 50 kHz / 2320.050 MHz ± 50 kHz on 13 cm band.

3. Design Concepts

The proposed 6-port feed consists of two independent radiating systems described below—see Figure 3. Septum polarizer design was performed by MICIAN [4] software. All other simulations were performed by CST Microwave Studio software [5].

3.1. 432 MHz (70 cm) Band

The 432 MHz feed is composed of two pairs of opposing bow-tie dipoles (A-A′, B-B′) responsible for vertical/horizontal polarization. These symmetrical dipoles are placed approximately λ/4 above a circular ground plane. The dipoles are fed by 50 Ω coaxial lines which are designed to mechanically and electrically match to 7/16′′ DIN style connectors, located on the bottom side of the ground plane, that are filled with PTFE to handle very high power. No impedance transformation between connectors and dipoles is required (Figure 4). This arrangement allows direct grounding of the connectors to the ground plane with four screw fasteners. Symmetry is maintained with the outer shell of carrier pipes, which function as a sleeve balun [6, 7]. For all polarization states, each pair of dipoles is excited by an external 3 dB Wilkinson power divider and 180 degree phase shifter, since dipole feed orientation is swapped in order to improve radiation pattern symmetry and minimize the supply line lengths.

3.2. 2320 MHz (13 cm) Band

The 2320 MHz dual-port (LHC/RHC) feed is based on our previous research work dealing with septum polarizers [810], see also [11, 12]. Using CST software simulation, we found that conversion to circular polarization using a 5-step septum occurs at virtually 100% efficiency [9]. To obtain good pattern symmetry, suppression of side lobes, and separation of cross-polarization, a dual-mode (HE11) Potter-style horn [1315] equipped with a septum polarizer has been chosen [15]—see Figure 5. The transition between coaxial feed line and waveguide is achieved by using conical probes [9]. The circular ground plane functionally performs as a choke [16] having diameter D2 and height of rim HR. The choke effect is to slightly modify the Potter horn’s radiation pattern causing a small decrease in the feed boresight, thus providing a slight performance improvement in our prime-focus feed-configured antenna [1, 10]. The ground plane provides for placement of the 432 MHz dipoles as well.

Main design dimensions of the proposed feed are summarized in Table 1; and indicate wavelengths at center of respective band.

Very important is distance  mm, that is, phase center position of the 2320 MHz feed above the ground plane. It was designed to achieve flush positions for both phase centers.

4. Results

4.1. Simulated 3D Radiation Patterns

3D radiation patterns from CST are shown in Figure 6 for 432 MHz and Figure 7 for 2320 MHz. The symmetric patterns show low cross-polarization for both bands. Note the location of the phase centers (red points). For both the 432 MHz and 2320 MHz bands, the calculated phase centers are located ±1 mm at the aperture plane (dimension HR).

A feed prototype (Figures 8 and 9) was fabricated from aluminum alloy and was measured in the anechoic chamber at ERA company [17]. The feed’s weight is about 5 kg.

4.2. Measured Radiation Pattern for 432 MHz

Since vertical and horizontal polarization pattern symmetry is excellent, the measured radiation pattern cut of H plane horizontal polarization is identical to the cut of E plane vertical polarization and vice versa. See Figure 10 for both polarization states. Note the very low cross-polarization level at the main lobe (suppression < −25 dB).

4.3. Measured Radiation Pattern for 2320 MHz

Measurement of only one polarization state (RHC) was performed with and without the 432 MHz section acting as a choke (Figure 11). Its effect may be seen as a slight decrease in the main lobe, reducing blockage effects and improving the overall efficiency. However, the choke subtly increases backward radiation. The simulated Axial Ratio (AR) parameter is better than 0.1 dB in the boresight direction. No special measurement of AR has been performed, since our previous results showed very low AR for a similar feed [10]. Such feed with scaled dimensions operates at 1296 MHz with a measured Axial Ratio better than 0.3 dB. So the Axial Ratio <0.3 dB (no choke) and <0.6 dB (with choke) for the proposed 2320 MHz feed section in the boresight direction can be expected.

4.4. Return Loss for 432 MHz Band

Return loss for this band was measured behind the Wilkinson power divider to eliminate its influence on the measurement. Two Mini-Circuits directional couplings, ZFDC—10-2-S, connected to the appropriate dipole were used for this measurement. The feed was excited by an Agilent E8257D signal generator. Output level was measured with a Wiltron 37347A spectrum analyzer. Calculated and measured results are shown in Figure 12. For each case, one set of respective dipoles (A-A′ or B-B′, see Figure 3) was simultaneously excited with 0 or 180° mutual phase-shift, realized by a different length of feeding cables.

4.5. Return Loss for 2320 MHz Band

A Wiltron 37347A vector analyzer was used for these measurements. Very good impedance match throughout a wide bandwidth was observed (Figure 13); however, for EME, fractional bandwidth of only about 1% around 2320 MHz is required. The differences between receiving (Rx) and transmitting (Tx) ports are attributed to dissimilar connector types at the ports. While the Rx port uses an N style connector, the Tx port employs a 7/16′′ DIN connector because of its power handling capability.

5. Practical Experience

Antenna Rx performance was tested using Sun versus cold sky comparisons on both bands, see Figures 14 and 15. On 432 MHz, a LNA with noise figure of 0.2 dB was used. On 2320 MHz, a LNA with noise figure of 0.45 dB was used. A solar flux level of 112 sfu was present for all measurements.

An average Sun noise to cold sky ratio of 14 dB was achieved for the 432 MHz band. A Sun noise to cold sky ratio of 17 dB was achieved for the 2320 MHz band.

There exists further opportunities for performance improvement, mainly by reducing cable lengths between the feed connectors and the LNAs.

6. Conclusion

A compact, dual-band feed was designed for very low-noise applications and was successfully tested for Earth-Moon-Earth operation. Antenna efficiency was evaluated by the EME Performance Calculator [18]. Reasonable values of 47% (40.5 dBi) 2320 MHz and 55% (26.64 dBi) 432 MHz based on Sun versus cold sky measurement were obtained. The lower efficiency on 2320 MHz is attributed to slight deviations from the parabolic shape of the reflector. With butterfly-shaped dipoles used for 432 MHz band, very good impedance matching was achieved over a wide frequency range and also the required parameters for power handling were satisfied.

Acknowledgments

The authors would like to thank Robert Valenta for discussions. This paper has been created under the COST IC1102 VISTA action and partially supported by the COST LD 12055 AMTAS (Advanced Modeling and Technologies for Antennas and Sensors).