Tomas Kohout, Antti Näsilä, Tuomas Tikka, Mikael Granvik, Antti Kestilä, Antti Penttilä, Janne Kuhno, Karri Muinonen, Kai Viherkanto, Esa Kallio VTT Technical.

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Tomas Kohout, Antti Näsilä, Tuomas Tikka, Mikael Granvik, Antti Kestilä, Antti Penttilä, Janne Kuhno, Karri Muinonen, Kai Viherkanto, Esa Kallio VTT Technical Research Centre of Finland Aalto University, Espoo, Finland Department of Physics, University of Helsinki, Finland Reaktor Space Lab Ltd Institute of Geology, The Czech Academy of Sciences, Prague, Czech Republic

AIDA-ASPECT

ASPECT 3 unit CubeSat equipped with a spectral imager/spectrometer Propulsion Avionics Radiation-hardened platform Payload: VIS-NIR spectral imager Semi-autonomous navigation and operations Aalto-1 and Aalto-2 heritage (launched June 2017) Better than 2 m spatial resolution from 4 km Didymos orbit Didymoon Didymain ASPECT

Payload concept 1U envelope 3 measurement channels: VIS (500–900 nm) spectral imager (614 x 614 pixels) NIR (900–1600 nm) spectral imager (256 x 256 pixels) SWIR (1600–2500 nm) spectrometer (1 pixel) Aalto-1 Spectral Imager heritage Based on VTT’s tunable filter technology (Fabry-Perot Interferometers) Freely selectable wavelength bands On-board data processing

ASPECT technical objectives AT1 Demonstration of CubeSat autonomous operations in deep space environment AT2 Navigation in the vicinity of a binary asteroid AT3 Demonstration of satellite survival during impact AT4 Demonstration of joint spacecraft – CubeSat operations AT5 Demonstration of spectral imaging of asteroid materials

ASPECT scientific objectives  ASPECT scientific objectives and results AS1 Map the surface composition of the Didymos system Result Composition and homogeneity of the Didymos asteroid, changes as a result of DART impact Information on the origin and evolution of the Didymos binary system AS2 Photometric observations and modeling of the Didymos system under varying phase angle and distance Surface particle size distribution and composition for Didymos II and Didymos I (simultaneous modeling of photometry and spectroscopy) AS3 Evaluate space weathering effects on Didymos II by comparing mature and freshly exposed material Information on the surface processes on airless bodies due to their exposure to the interplanetary environment AS4 Identify local shock effects on Didymos II based on spectral properties of crater interior Information on the processes related to impacts on small Solar System bodies AS5 Observations of the plume produced by the DART impact Evolution and composition of the DART impact plume AS6 Map global fallback ejecta on Didymos II and Didymos I Detailed global mapping of fallback ejecta on both Didymos I and Didymos II

DART impact, crater and ejecta distribution ESA Gaffey 2010

Space weathering Binzel et al. 2010

Space weathering Material damage/response to interplanetary environment (solar wind, microimpacts, space radiation) Spectral changes associated with presence of reduced iron nanoparticles Confirmed on the Moon and Itokawa Vesta may have distinct space weathering mechanism Itokawa - Noguchi et al. 2011

Hydrated features Bus et al. 1999

Shock effects Kohout et al. 2014

Shock effects Shock-darkened or melted material has spectra similar to C/X-complex asteroids. Can these be related?

Conclusions ASPECT is a 3U asteroid CubeSat with an VIS-NIR imaging spectrometer ASPECT observations will complement these of AIM ASPECT will provide high resolution image and spectral coverage of Didymos ASPECT will provide insight into space weathering and impacts on asteroids