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Radio Science Investigation with AIM

The Asteroid Impact Mission (AIM) is a candidate ESA mission to the binary Near-Earth Asteroid (65803) Didymos. While its main objective is to demonstrate new technologies for future deep-space missions, AIM will also characterise for the first time a binary asteroid system, providing an understanding of its formation and of the origin of the Solar System.

Italy

16-M-06-01

University of Bologna
Assessment of an Anchoring Device for CubeSat Landers

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.

Romania

16/701

Institute of Space...
System analysis of deployable components for micro landers in low gravity environment

The project entitled "System analysis of deployable components for micro landers in low gravity environment" is conducted within the framework of the ESA contract no. 4000117150/16/NL/HK/hh. Its goal is to perform an analysis and trade-off between the various design options for antennas and solar array deployment mechanisms (including a comparison between the fixed and deployable configurations) of the MASCOT-2 lander in the micro-gravity environment of Didymoon.

Poland

15/725

Space Research Centre of...
Assessment Study of Autonomous Optical Navigation for an Asteroid Impact Mission

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.

Denmark

16-M-06-02

TECHNICAL UNIVERSITY OF...

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