2018
DOI: 10.1016/j.actaastro.2018.06.044
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An investigation of millimeter wave reflectarrays for small satellite platforms

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Cited by 3 publications
(4 citation statements)
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“…5. It is important to mention that the phase range also depends on the substrate's thickness where an electrically thick substrate provides a wideband operation but at the same time will limit phase swing [52,53]. For instance, a substrate thickness of šœ†/10 gives a phase reflection range of approximately 300Ā° [44].…”
Section: A Multi-resonance Approachmentioning
confidence: 99%
“…5. It is important to mention that the phase range also depends on the substrate's thickness where an electrically thick substrate provides a wideband operation but at the same time will limit phase swing [52,53]. For instance, a substrate thickness of šœ†/10 gives a phase reflection range of approximately 300Ā° [44].…”
Section: A Multi-resonance Approachmentioning
confidence: 99%
“…For the satellite cluster system in this paper, all the satellites are equipped with electronically steerable directive antennas, which can achieve highā€speed directional transmitting and receiving between satellites at the mmWave band. According to ITUā€R S.1327 24,28 and taking the actual antenna model for mmWave small satellites as references, 29ā€30 the reference antenna radiation pattern of the LEO interā€satellite system around 60 GHz can be characterized by the following equations: Gtxfalse/rxfalse(Ī¾h,Ļ‰false)={leftarrayGmaxāˆ’3(2Ļ‰/Ī¾h)2forĻ‰ā‰¤aĪ¾h/2arrayGmaxāˆ’20foraĪ¾h/2<Ļ‰ā‰¤bĪ¾h/2arrayGmaxāˆ’25log(2Ļ‰/Ī¾h)forbĪ¾h/2<Ļ‰ā‰¤Ī¾1array0forĪ¾1<Ļ‰ where G tx / rx is the gain at the angle Ļ‰ from the main beam direction in units of dBi. Ī¾ h denotes halfā€power beamwidth in units of degrees, and Ī¾ 1 is the value of Ī¾ when G tx / rx in equation Gtxfalse/rx=Gmaxāˆ’25normallogfalse(2Ļ‰false/Ī¾hfalse) equals to 0 dBi.…”
Section: System Model and Problem Formulationmentioning
confidence: 99%
“…Moreover, the radiation pattern and gain performance of the mmWave satellite antenna can be obtained via simulation and measurement in prior, 30 so the antenna patterns are assumed to be known in this paper.…”
Section: System Model and Problem Formulationmentioning
confidence: 99%
“…Therefore, it is very important to explore alternative approaches to enable lightweight high-gain antennas that occupy a considerably small fraction of the payload and volume of SmallSats. There have been a handful of initiatives in realizing high-performance lightweight antennas for small satellites 1ā€“3 including Fabry-PĆ©rot cavity antennas 4 , deployable mesh reflectors 5,6 , inflatable balloon reflectors 7 , deployable waveguide slot antennas 8 , and reflectarrays 9 .…”
Section: Introductionmentioning
confidence: 99%