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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...
Assessment of a Low Velocity PicoSat Orbital Deployer for AIM and Interplanetary Missions

The output of the activity should show the necessary engineering changes to an existing CubeSat deployer to meet AIM mission and system requirements and prepare an appropriate interface definition for accommodation on the AIM spacecraft including among others:
- Identification of the requirements for a LV-POD in an interplanetary environment, first addressing the needs of AIM and extending to generic interplanetary missions.
- Review of technology to extend existing CubeSat deployment systems and identification of their limitations.

The Netherlands

15/M63

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