In the following the list of some of the documents produced during the research on aerospace topics.

Other documents, such as technical reports and deliverables, are not reported because confidential.

 

Papers

Minotti, A. “A new NANOSATs propulsion system: swirling-combustion chamber and water electrolysis“, AIMS Energy, 6(3): 402–413; DOI: 10.3934/energy.2018.3.402.

Pallone, M., Pontani, M., Teofilatto, P. and Minotti, A. “Design Methodology and Performance Evaluation of New Generation Sounding Rockets”, International Journal of Aerospace Engineering, vol. 2018, 1678709. doi:10.1155/2018/1678709.

Minotti, A. “Academic outreach in non-proliferation: the Dual Space System technical course”, proceedings of the 1ST Scientific International Conference on CBRNE, Rome, Italy, 22 May 2017.

Minotti, A. “ A micro-propulsion system to widen CubeSats applications to security”, proceedings of the 1ST Scientific International Conference on CBRNE, Rome, Italy, 22 May 2017.

Petrella, P., Teofilatto, P. and Minotti, A. “Dynamic Separation in Air Launch: A Model”, IAACU-13-08-04, 2nd IAA Conference on University Satellite Missions and Cubesat Workshop, 4-9 February, 2013, Rome, Italy.

Minotti, A. “O2/CH4 kinetic mechanisms for Aerospace Applications at low pressure and temperature, validity ranges and comparison”. Aeronautics and Astronautics, InTech, ISBN-978-953-307-473-3, chapter 13, pp. 369-400, 2011.
Minotti, A. and Bruno, C.,“Comparison Between Simulations of Real and Ideal LRE Combustion of LO2-CH4”, Recent Patents on Space Technology, Vol. 2, 2010, 1-9.

Minotti, A. and Bruno, C., “Comparison between Real and Ideal Sub and Supercritical Combustion Simulations for LO2-CH4 LRE at 15MPa”, 46th AIAA Aerospace Science Meeting and Exhibit, AIAA-2008-0951, RENO, Nevada, 7-10 January 2008.

Minotti, A. and Bruno, C., “Comparison between Supercritical Combustion Modelling for LO2-CH4 Rocket Engines at 15MPa and 16.5MPa using Real and Ideal gas properties”, Space Propulsion 2008 proceedings: 5th International Spacecraft Propulsion Conference & 2° International Symposium on Propulsion for Space Transportation, s24_095, 5-8 May 2008, Heraklion, Crete.

Minotti, A. and Bruno, C., “Flame temperatures in non-premixed flames”, AIAA Aerospace Science Meeting and Exhibit, AIAA-2008-0998, RENO, Nevada, 7-10 January 2008.

Minotti, A. and Bruno, C., “Sub-Trans and Supercritical Properties for LO2-CH4 at 15MPa”, AIAA Journal of Thermophysics and Heat Transfer, Vol. 21, issue 4, 796-810, 2007.

Minotti, A. and Bruno, C., “Comparison between Subcritical Combustion Modelling for LO2-CH4 Rocket Engines at 15MPa using Real and Ideal gas properties”, EUCASS 07 proceedings, 1-6 July 2007, Brussels.

Minotti, A. and Bruno, C., “Comparison between Supercritical Combustion Modelling for LO2-CH4 Rocket Engines at 15MPa using Real and Ideal gas properties”, CEAS 2007 proceedings,2007-031, 10-13 September 2007, Berlin.