TY - JOUR
T1 - Development of a laser power beaming demonstration for CLPS landers
AU - Centers, Ross
AU - Schertz, Joshua
AU - Purrington, Curtis
AU - Dickson, David
AU - Kezer, Loren
AU - Janikowski, Adam
AU - Schmit, John
AU - Broslav, Timofey
AU - Hinton, Jef
AU - Sowers, George
AU - Vance, Leonard
AU - Kalita, Himangshu
AU - Diaz-Flores, Alvaro
AU - Fernandez, Jose
AU - Thangavelautham, Jekan
N1 - Publisher Copyright: © 2020 by the International Astronautical Federation (IAF). All rights reserved.
PY - 2020
Y1 - 2020
N2 - Laser based power transmission represents an enabling technology for moving power from energy rich regions to areas of high demand, while being able to overcome the dramatic topography of the lunar poles [1-4]. To provide the earliest opportunity for flight demonstration of this critical technology, we have designed and conducted relevant environment testing of a low power, minimal mass laser power beaming demonstrator that can be mounted as an ancillary payload on a NASA Commercial Lunar Payload Services (CLPS) lander. Our entire system consists of a laser, beam director, target identification system, and multiple FemtoSat receivers [5]. This integrated system is able to test key objectives incrementally. We plan to test methods of ejecting and locating the receiver on the lunar surface, pointing and aiming the laser at the receiver, and powering the receiver. We have tested key components of the system and are moving toward integrated tests.
AB - Laser based power transmission represents an enabling technology for moving power from energy rich regions to areas of high demand, while being able to overcome the dramatic topography of the lunar poles [1-4]. To provide the earliest opportunity for flight demonstration of this critical technology, we have designed and conducted relevant environment testing of a low power, minimal mass laser power beaming demonstrator that can be mounted as an ancillary payload on a NASA Commercial Lunar Payload Services (CLPS) lander. Our entire system consists of a laser, beam director, target identification system, and multiple FemtoSat receivers [5]. This integrated system is able to test key objectives incrementally. We plan to test methods of ejecting and locating the receiver on the lunar surface, pointing and aiming the laser at the receiver, and powering the receiver. We have tested key components of the system and are moving toward integrated tests.
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M3 - Conference article
SN - 0074-1795
VL - 2020-October
JO - Proceedings of the International Astronautical Congress, IAC
JF - Proceedings of the International Astronautical Congress, IAC
T2 - 71st International Astronautical Congress, IAC 2020
Y2 - 12 October 2020 through 14 October 2020
ER -