1. Aerothermodynamic and feasibility study of a deployable aero-braking re-entry capsule;Savino;Fluid Dyn. Mater. Process.,2012
2. V. Carandente, G. Elia, R. Savino, Conceptual design of de-orbit and re-entry modules for standard CubeSats, in: Proceedings of the 2nd IAA Conference on University Satellite Missions and Cubesat Workshop, Rome, February 4–7, 2013.
3. Aerothermodynamic and stability analyses of a deployable re-entry capsule;Carandente;Acta Astronaut.,2014
4. New concepts of deployable de-orbit and re-entry systems for CubeSat miniaturized satellites;Carandente;Recent Pat. Eng.,2014
5. MISTRAL Research Project: Proposal for the Aerospace Campania District, DAC feasibility study, 2012.