TY - GEN
T1 - Lunar cubesat lander to explore mare tranquilitatis pit
AU - Kalita, Himangshu
AU - Thangavelautham, Jekan
N1 - Funding Information: The authors would like to thank Dr. Mark Robinson from Arizona State University for his invaluable input in the development of Arne-II CubeSat lander concept, and the contributions of Aman Chandra, Steven Morad, Ravi Nallapu, Rachel Moses, and Jasem Amoudi for their contributions in the design of Arne-II. Publisher Copyright: © 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2020
Y1 - 2020
N2 - The Lunar Gateway is expected to be positioned on-orbit around the Moon or in a Halo orbit at the L2 Lagrange point. The proposed Lunar Gateway is a game-changer for enabling new science utilizing CubeSats and presents a refreshing new opportunity for utilization of these small spacecraft as explorers. We propose to develop a Lunar CubeSat Lander that will be deployed from the Lunar Gateway Logistics Module (presumed to be at L2) to perform science and exploration of the lunar surface. The CubeSat lander will land near Mare Tranquilitatis to determine the extent of the void and identify the presence of volatile resources including water in its regolith. The CubeSat lander is a 27U with stowed dimensions of 34 cm×35 cm×36 cm and mass of 54 kg. It will be deployed from the Lunar Gateway and perform a lunar orbit insertion by using its onboard High-Performance Green Propulsion (HPGP) system followed by descent maneuver to get into a 25 km altitude from the lunar surface. From there, the lander will get into a powered descent maneuver over Mare Tranquilitatis taking 4-6 minutes. Onboard visual navigation will be used to land on the Mare Tranquilitatis Region by rapidly firing the descent thrusters. The lander is equipped with a Volatile Analysis by Pyrolysis of Regolith (VAPoR) instrument to perform pyrolysis and mass spectrometry of lunar regolith. Moreover, it will carry three spherical hopping robots (SphereX) that will hop inside the pit to perform mapping and electrical impedance spectroscopy of regolith inside the pit to determine the presence to water.
AB - The Lunar Gateway is expected to be positioned on-orbit around the Moon or in a Halo orbit at the L2 Lagrange point. The proposed Lunar Gateway is a game-changer for enabling new science utilizing CubeSats and presents a refreshing new opportunity for utilization of these small spacecraft as explorers. We propose to develop a Lunar CubeSat Lander that will be deployed from the Lunar Gateway Logistics Module (presumed to be at L2) to perform science and exploration of the lunar surface. The CubeSat lander will land near Mare Tranquilitatis to determine the extent of the void and identify the presence of volatile resources including water in its regolith. The CubeSat lander is a 27U with stowed dimensions of 34 cm×35 cm×36 cm and mass of 54 kg. It will be deployed from the Lunar Gateway and perform a lunar orbit insertion by using its onboard High-Performance Green Propulsion (HPGP) system followed by descent maneuver to get into a 25 km altitude from the lunar surface. From there, the lander will get into a powered descent maneuver over Mare Tranquilitatis taking 4-6 minutes. Onboard visual navigation will be used to land on the Mare Tranquilitatis Region by rapidly firing the descent thrusters. The lander is equipped with a Volatile Analysis by Pyrolysis of Regolith (VAPoR) instrument to perform pyrolysis and mass spectrometry of lunar regolith. Moreover, it will carry three spherical hopping robots (SphereX) that will hop inside the pit to perform mapping and electrical impedance spectroscopy of regolith inside the pit to determine the presence to water.
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U2 - 10.2514/6.2020-2163
DO - 10.2514/6.2020-2163
M3 - Conference contribution
SN - 9781624105951
T3 - AIAA Scitech 2020 Forum
BT - AIAA Scitech 2020 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Scitech Forum, 2020
Y2 - 6 January 2020 through 10 January 2020
ER -