• Home
  • Current congress
  • Public Website
  • My papers
  • root
  • browse
  • IAC-21
  • B4
  • 9-GTS.5
  • paper
  • The GreenCube CubeSat mission: Development and Qualification of an autonomous Microgreens Cultivation System and demonstration of CubeSat propulsion in MEO

    Paper number

    IAC-21,B4,9-GTS.5,5,x66431

    Author

    Mr. Paolo Marzioli, Italy, Sapienza University of Rome

    Coauthor

    Mr. Diego Amadio, Italy, Sapienza - University of Rome

    Coauthor

    Mr. Federico Curianò, Italy, Sapienza University of Rome

    Coauthor

    Dr. Luca Gugliermetti, Italy, Sapienza University of Rome

    Coauthor

    Mr. Alessandro Moretti, Italy, University of Rome “La Sapienza”

    Coauthor

    Mr. Ludovico Gregori, Italy, University of Rome “La Sapienza”

    Coauthor

    Mr. Alessio Bergami, Italy, Sapienza University of Rome

    Coauthor

    Ms. Michela Boscia, Italy, Sapienza University of Rome

    Coauthor

    Mr. Sidhant Kumar, Italy, Sapienza University of Rome

    Coauthor

    Prof. Stefania De Pascale, Italy, University of Naples "Federico II"

    Coauthor

    Dr. Eugenio Benvenuto, Italy, ENEA - Italian National Agency for New Technologies, Energy and Sustainable Economic Development

    Coauthor

    Dr. Luca Nardi, Italy, ENEA - Italian National Agency for New Technologies, Energy and Sustainable Economic Development

    Coauthor

    Dr. Antonio Pannico, Italy, University of Naples "Federico II"

    Coauthor

    Mr. Christoph Montag, Germany, Institute of Space Systems, Universität Stuttgart

    Coauthor

    Mr. Giulio Metelli, Italy, ENEA - Italian National Agency for New Technologies, Energy and Sustainable Economic Development

    Coauthor

    Mr. Felix Schäfer, Germany, Institute of Space Systems, Universität Stuttgart

    Coauthor

    Prof.Dr. Georg Herdrich, Germany, Institute of Space Systems, University of Stuttgart

    Coauthor

    Mr. Clemens Berger, Germany, Institute of Space Systems, Universität Stuttgart

    Coauthor

    Prof. Rene Laufer, Sweden, Luleå University of Technology

    Coauthor

    Ms. Silvia Mari, Italy, ASI - Italian Space Agency

    Coauthor

    Dr. Marta Del Bianco, Italy, Italian Space Agency (ASI)

    Coauthor

    Dr. Gabriele Mascetti, Italy, Italian Space Agency (ASI)

    Coauthor

    Dr. Fabrizio Piergentili, Italy, Sapienza University of Rome

    Coauthor

    Prof. Fabio Santoni, Italy, Sapienza University of Rome

    Coauthor

    Mr. Lorenzo Frezza, Italy, Sapienza University of Rome

    Year

    2021

    Abstract
    The development and testing of next generation Environmental Control and Life Support Systems (ECLSSs) will support the future long-term manned mission in Lunar and, successively, Mars environments. In this perspective, performing biological experiments on miniaturized satellite platforms can provide an easy access to Space testing with extremely short development cycles.
    The GreenCube mission aims at demonstrating the effectiveness of a fully autonomous system to cultivate plants to early development stage (microgreens) in-orbit. The mission has obtained a free launch opportunity, offered by ESA, on-board the maiden VEGA-C launch in Medium Earth Orbit (MEO). The mission has been conceived by an Italian research group led by Sapienza University of Rome, together with ENEA (Italian National Agency for New Technologies, Energy and Sustainable Economic Development) and University of Naples Federico II, with the support and coordination  of the Italian Space Agency (ASI). The implementation of the experimental propulsive attitude control system has been made possible thanks to an international collaboration with University of Stuttgart, Germany.
    GreenCube is a 3U CubeSat (300 x 100 x 100 mm) and will operate on a 6000 km-high circular orbit. The design includes a plant cultivation unit of approximately two CubeSat units in size. The remaining unit is used for a commercial bus, including an experimental attitude control systems based on electric propulsion. The latter will be in-orbit demonstrated as a convenient and innovative method for maintaining a constant satellite spin rate and applied as a back-up attitude control system.
    The system will acquire microgreen growth/health and environmental data through multiple sensors. Meanwhile, actuators will regulate plants nutrition, inner unit temperature and air circulation during the cultivation phase. The complete microgreen production cycle is normally between 15 and 20 day long.  GreenCube will provide important information enabling a broader utilization of nano-satellites for biological systems testing and in-orbit plant cultivation in the near future. Furthermore, the technologies adopted in GreenCube and demonstrated in MEO could be easily applied to future CubeSat scientific missions.
    This paper will focus on the development and subsystem-level qualification of the 3U CubeSat GreenCube. The mission and general features of the CubeSat design will be described. Moreover, the plant unit and the on-board technologies will be illustrated. Finally, the testing activities performed for preliminary qualification will be reported.
    Abstract document

    IAC-21,B4,9-GTS.5,5,x66431.brief.pdf

    Manuscript document

    IAC-21,B4,9-GTS.5,5,x66431.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.