Light Italian CubeSat for Imaging of Asteroids (LICIACube, ) is a six-unit CubeSat of the Italian Space Agency (ASI). LICIACube is a part of the Double Asteroid Redirection Test (DART) mission and carries out observational analysis of the Didymos asteroid binary system after DART's impact on Dimorphos. It communicates directly with Earth, sending back images of the ejecta and plume of DART's impact as well as having done asteroidal study during its flyby of the Didymos system from a distance of , 165 seconds after DART's impact. LICIACube is the first purely Italian autonomous spacecraft in de
Light Italian CubeSat for Imaging of Asteroids (LICIACube, ) is a six-unit CubeSat of the Italian Space Agency (ASI). LICIACube is a part of the Double Asteroid Redirection Test (DART) mission and carries out observational analysis of the Didymos asteroid binary system after DART's impact on Dimorphos. It communicates directly with Earth, sending back images of the ejecta and plume of DART's impact as well as having done asteroidal study during its flyby of the Didymos system from a distance of , 165 seconds after DART's impact. LICIACube is the first purely Italian autonomous spacecraft in deep space. Data archiving and processing is managed by the Mission Control Center of Argotec. Its mission ended in the autumn of 2022.
== History == LICIACube is the first deep space mission developed and autonomously managed by an Italian team. To collaborate upon the design, integration, and testing of the CubeSat, the Italian Space Agency selected the aerospace company Argotec, while the LICIACube GS has a complex architecture based on a mission control center in Turin hosted by Argotec and science operation center in Rome. Antennas of the NASA Deep Space Network (NASA DSN) and data archiving and processing is managed at the ASI SSDC. The scientific team making this cubesat is led by National Institute of Astrophysics INAF (OAR, IAPS, OAA, OAPd, OATs) with the support of IFAC-CNR and Parthenope University of Naples. The team is supported by the University of Bologna for orbit determination and satellite navigation and the Polytechnic University of Milan, for mission analysis and optimisation. The LICIACube team includes the wider Italian scientific community involved in the definition of all the aspects of the mission: trajectory design; mission definition (and real-time orbit determination during operations); impact, plume and imaging simulation, and modelling, in preparation of a suitable framework for the analysis and interpretation of in situ data. Major technological challenges during the mission (autonomous targeting and imaging of such a small body during a fast flyby with the limited resources of a CubeSat) is affordable thanks to cooperation between the mentioned teams in support of the engineering tasks.
Discovered by embedding cosine similarity (sentence-transformers MiniLM, 384-dim).