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The current study has evaluated the feasibility of a CubeSat anchoring device in the context of AIM mission. By enabling this capability on a Cubesat type nanosatellite, the overall AIM mission will be further augmented with in-situ scientific measurements such as close surface visual observations, on site plume ejecta monitoring, impact induced accelerations and seismic wave propagated through asteroid body, etc. Moreover, the anchoring device has a strong reuse potential in the context of SSA by the utilisation of Cubesats or small platforms for debris removal techniques.
Institute of Space...
The Asteroid Impact Mission (AIM) is part of the Asteroid Impact and Deflection Assessment (AIDA). The intention of AIDA is to send two spacecraft, AIM and Double Asteroid Redirection Test (DART) to the binary asteroid 65803 Didymos, to investigate the kinetic effects of crashing an impactor spacecraft into the smaller body of the binary asteroid, hereafter called Didymoon. The large body is called Didymain. Ultimately the mission hopes to test whether a spacecraft could successfully deflect an asteroid on collision course with Earth.
TECHNICAL UNIVERSITY OF...