2021
DOI: 10.1142/s2251171721500100
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Laboratory Demonstration of the Local Oscillator Concept for the Event Horizon Imager

Abstract: Black hole imaging challenges the third-generation space VLBI, the Very Long Baseline Interferometry, to operate on a 500[Formula: see text]GHz band. The coherent integration time needed here is 450[Formula: see text]s though the available space oscillators cannot offer more than 10[Formula: see text]s. Self-calibration methods might solve this issue in an interferometer formed by three antenna/satellite systems, but the need for the third satellite increases the mission costs. A frequency transfer is of speci… Show more

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Cited by 4 publications
(2 citation statements)
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“…TriHex relies on the Upper Side Band Syntonization (USBS) concept described for two spacecraft in [37] but extended to N=3 spacecraft [38]. The USBS concept was successfully demonstrated in the ESTEC RF Laboratory [39]. For synchronization TriHex relies on spatial symmetry, in practice realized by (a) manufacturing identical circuits with phase similarity to within 117° at 250 MHz, (b) cutting optical fibres with 3-millimetre accuracy and (c) having the spacecraft in relative navigation with an accuracy of 1 cm.…”
Section: Some Technical Featuresmentioning
confidence: 99%
“…TriHex relies on the Upper Side Band Syntonization (USBS) concept described for two spacecraft in [37] but extended to N=3 spacecraft [38]. The USBS concept was successfully demonstrated in the ESTEC RF Laboratory [39]. For synchronization TriHex relies on spatial symmetry, in practice realized by (a) manufacturing identical circuits with phase similarity to within 117° at 250 MHz, (b) cutting optical fibres with 3-millimetre accuracy and (c) having the spacecraft in relative navigation with an accuracy of 1 cm.…”
Section: Some Technical Featuresmentioning
confidence: 99%
“…The accurate positioning of the satellites and interchange of local oscillator signals permit the phase calibration of EHI observations and, thus, the use of complex visibilities (Kudriashov et al 2021b). Both the proposed on-the-fly positioning and the on-board data processing require a working inter-satellite link (ISL) to perform highly accurate ranging measurements, as well as to exchange observed signals and local oscillator components for coherent operation (Martin-Neira et al 2019;Kudriashov et al 2021a). This implies a direct line of sight between the satellites.…”
mentioning
confidence: 99%