urn:nasa:pds:context:instrument_host:spacecraft.liciacube 1.3 1.22.0.0 Product_Context Light Italian CubeSat for Imaging of Asteroids (LICIACube) Spacecraft 2026-07-07 1.3 Removed duplicate Internal_Reference entries from Reference_List. 2024-12-18 1.2 Updated schema version. Adding missing "investigation" references. Description updated. 2023-12-28 1.1 RChen added naif_host_id and instruments hga, leia, luke 2021-08-12 1.0 Created by A.C.Raugh from information downloaded from the public DART mission website maintained by the Applied Physics Laboratory at Johns Hopkins University (JHU APL) on 2021-08-12. urn:nasa:pds:context:investigation:mission.double_asteroid_redirection_test instrument_host_to_investigation urn:nasa:pds:context:instrument:liciacube.hga instrument_host_to_instrument urn:nasa:pds:context:instrument:liciacube.leia instrument_host_to_instrument urn:nasa:pds:context:instrument:liciacube.luke instrument_host_to_instrument urn:nasa:pds:context:investigation:mission.light_italian_cubesat_for_imaging_of_asteroids instrument_host_to_investigation The Light Italian CubeSat for Imaging of Asteroids (LICIACube) Spacecraft Spacecraft LICIA The LICIACube was a six-unit cubesat (measuring 10cm x 20m x 30cm) with two light solar arrays, autonomous attitude control; an propulsion system, and two cameras in its scientific payload. It road along on the DART spacecraft to the encounter with the (65803) Didymos system, separating 15 days before impact in order to observe the collision and send images back to Earth. The LICIACube was designed and manufactured in Italy.