Meteoroids detection with the LUMIO lunar CubeSat

被引:7
|
作者
Topputo, F. [1 ]
Merisio, G. [1 ]
Franzese, V. [1 ]
Giordano, C. [1 ]
Massari, M. [1 ]
Pilato, G. [2 ]
Labate, D. [2 ]
Cervone, A. [3 ]
Speretta, S. [3 ]
Menicucci, A. [3 ]
Turan, E. [3 ]
Bertels, E. [4 ]
Vennekens, J. [5 ]
Walker, R. [5 ]
Koschny, D. [5 ,6 ]
机构
[1] Politecn Milan, Dept Aerosp Sci & Technol, Via Masa 34, I-20156 Milan, Italy
[2] Leonardo SpA, Via Officine Galileo 1, I-50013 Campi Bisenzio, Firenze, Italy
[3] Delft Univ Technol, Kluyverweg 1, NL-2629 HS Delft, Netherlands
[4] ISIS Innovat Solut Space, Motorenweg 23, NL-2623 CR Delft, Netherlands
[5] ESA, European Space Res & Technol Ctr ESTEC, Keplerlaan 1,, NL-2201 AZ Noordwijk, Netherlands
[6] Tech Univ Munich, Garching, Germany
关键词
LUMIO; Interplanetary CubeSat missions; Moon; Meteoroids; Impact flashes; IMPACT FLASHES; HYPERVELOCITY IMPACTS; LUMINOUS EFFICIENCY; FLUX; MOON; NAVIGATION;
D O I
10.1016/j.icarus.2022.115213
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
The Lunar Meteoroid Impacts Observer (LUMIO) is a CubeSat mission to observe, quantify, and characterize the meteoroid impacts on the lunar farside by detecting their flashes. This complements the knowledge gathered by Earth-based observations of the lunar nearside, thus synthesizing global information on the lunar meteoroid environment and contributing to the lunar situational awareness. The goal of LUMIO is to advance our current knowledge of meteoroid models in the solar system. In this work, we present the methodology devised to predict the scientific contribution of LUMIO. Our approach relies on combined modeling and simulation of payload, orbit, and environment. The analyses carried out have been used to drive the design of the LUMIO mission and its payload, the LUMIO-Cam. A payload radiometric model is derived and exploited to assess the quality of the scientific measurements. A dedicated study about straylight rejection is carried out to assess how straylight noise affects LUMIO-Cam measurements. Our results indicate that a 150 mm baffle grants good performance when the Sun angle is between 20 degrees and 90 degrees. Furthermore, the present-day LUMIO mission has the potential to detect more than 6000 impact flashes during the activity peak of the Geminids in 2024 in the range of the equivalent impact kinetic energy at Earth of [10-6,10-1] kton TNT Equivalent. Compared to previous programmes, LUMIO could refine information and fill the knowledge gap about the meteoroid population in the ranges of the equivalent impact kinetic energy at Earth of [10-6, 10-4] kton TNT Equivalent and [10-4, 10-1] kton TNT Equivalent, respectively.
引用
收藏
页数:19
相关论文
共 50 条
  • [41] Impact detection in space: Derivation of physical properties of meteoroids and debris
    Mandeville, J.C.
    Advances in Space Research, 17 (12):
  • [42] Lunar Lander and CubeSat-based Payload Antenna System for a Surface Wireless Local Network
    Miguelez-Gomez, Noemi
    Yepez, Sabrina A.
    Clayton, Ryan M.
    Roberts, Blake A.
    Korczyk, Dalton C.
    Henderson, Troy
    Rojas-Nastrucci, Eduardo A.
    2021 IEEE INTERNATIONAL CONFERENCE ON WIRELESS FOR SPACE AND EXTREME ENVIRONMENTS (WISEE), 2021,
  • [43] Preliminary Analysis of Delta-V Requirements for a Lunar CubeSat Impactor with Deployment Altitude Variations
    Song, Young-Joo
    Ho, Jin
    Kim, Bang-Yeop
    JOURNAL OF ASTRONOMY AND SPACE SCIENCE, 2015, 32 (03) : 257 - 268
  • [44] Design and characterization of a low cost CubeSat multi-band optical receiver to map water ice on the lunar surface for the Lunar Flashlight mission
    Vinckier, Quentin
    Crabtree, Karlton
    Paine, Christopher G.
    Hayne, Paul O.
    Sellar, Glenn R.
    INFRARED REMOTE SENSING AND INSTRUMENTATION XXV, 2017, 10403
  • [45] Nature of and Lessons Learned from Lunar Ice Cube and the First Deep Space Cubesat 'Cluster'
    Clark, Pamela
    MacDowall, Robert
    Farrell, William
    Brambora, Cliff
    Lunsford, Al
    Hurford, Terry
    Folta, David
    Malphrus, Benjamin
    Grubb, Matt
    Wilzcewski, Sarah
    Bujold, Emily
    CUBESATS AND NANOSATS FOR REMOTE SENSING II, 2018, 10769
  • [46] Optical and mechanical designs of the multi-band SWIR receiver for the Lunar Flashlight CubeSat mission
    Vinckier, Quentin
    Crabtree, Karlton
    Gibson, Megan
    Smith, Christopher
    Wehmeier, Udo
    Hayne, Paul O.
    Sellar, R. Glenn
    OPTICAL DESIGN AND ENGINEERING VII, 2018, 10690
  • [47] CubeSat Development for Lightning Flashes Detection: RaioSat Project
    Julio Filho, Antonio Cassiano
    Tikami, Auro
    Ferreira de Paula, Elaine de Souza
    Pineros, Jhonathan Murcia
    Fernandes, George Favale
    Pires Camargo, Lazaro Aparecido
    Monteiro Barbosa dos Santos, Carlos Alberto
    dos Santos, Walter Abrahao
    Naccarato, Kleber Pinheiro
    JOURNAL OF AEROSPACE TECHNOLOGY AND MANAGEMENT, 2020, 12 (12) : 80 - 93
  • [48] WILDFIRE DETECTION CUBESAT BASED ON CONVOLUTION NEURAL NETWORK
    Bin Azami, Muhammad Hasif
    Orger, Necmi Cihan
    Schulz, Victor Hugo
    Cho, Mengu
    SPIE FUTURE SENSING TECHNOLOGIES 2021, 2021, 11914
  • [49] EuroMir 95: detection of orbital debris and meteoroids in low Earth orbit
    Mandeville, J.C.
    Advances in Space Research, 1997, 19 (02) : 261 - 265
  • [50] Detection of the lunar body tide by the Lunar Orbiter Laser Altimeter
    Mazarico, Erwan
    Barker, Michael K.
    Neumann, Gregory A.
    Zuber, Maria T.
    Smith, David E.
    GEOPHYSICAL RESEARCH LETTERS, 2014, 41 (07) : 2282 - 2288