AIAA SCITECH 2023 Forum 2023
DOI: 10.2514/6.2023-1787
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Lift Wire Deployment and Anchoring System for the Lunar Crater Radio Telescope on the Far Side of the Moon

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“…The design of the LCRT antenna comprises a 350 m diameter parabolic reflector deployed in a crater with suitable depth-to-diameter ratio, via high-TRL crater-wall-climbing robots or anchoring systems and lift wires [7]. A dual linearly polarized and resonance-optimized log periodic dipole array (LPDA) antenna is employed as the feed/receiver element suspended at the reflector focus [35].…”
Section: Methodsmentioning
confidence: 99%
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“…The design of the LCRT antenna comprises a 350 m diameter parabolic reflector deployed in a crater with suitable depth-to-diameter ratio, via high-TRL crater-wall-climbing robots or anchoring systems and lift wires [7]. A dual linearly polarized and resonance-optimized log periodic dipole array (LPDA) antenna is employed as the feed/receiver element suspended at the reflector focus [35].…”
Section: Methodsmentioning
confidence: 99%
“…The design of a Lunar Crater Radio Telescope (LCRT) on the far side of the Moon has been proposed with the objective to measure the spectrum of the sky-averaged Dark Ages signal in the 4.7-47 MHz frequency range, which has not been explored for cosmological observations to date [4][5][6]. Using deployment technologies being developed at NASA Jet Propulsion Laboratory [7], a 350 m diameter parabolic reflector mesh will be deployed in a 1.3 km diameter lunar crater on the farside of the Moon [8], with a receiver suspended at its focus. An illustration of LCRT is shown in figure 1.…”
Section: Introductionmentioning
confidence: 99%