Design of interplanetary hybrid cubesat and smallsat propulsion systems ET Jens, AC Karp, J Rabinovitch, A Conte, B Nakazono, DA Vaughan 2018 Joint Propulsion Conference, 4668, 2018 | 30 | 2018 |
Characterization of PolyMethylMethAcrylate as a fuel for hybrid rocket motors J Rabinovitch, ET Jens, AC Karp, B Nakazono, A Conte, DA Vaughan 2018 Joint Propulsion Conference, 4530, 2018 | 20 | 2018 |
Design, Modeling and Testing of a O2/CH4 Igniter for a Hybrid Rocket Motor A Conte, J Rabinovitch, E Jens, A Chandler Karp, B Nakazono, ... 2018 Fluid Dynamics Conference, 3239, 2018 | 14 | 2018 |
Development Testing of Hybrid Rocket Motors Using Classical Fuels for Interplanetary CubeSats ET Jens, AC Karp, S Contadin, A Conte, B Nakazono, D Vaughan 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 4981, 2017 | 9 | 2017 |
Dual-bell nozzle for space launchers with fluidic control of transition A Ferrero, A Conte, E Martelli, F Nasuti, D Pastrone AIAA Propulsion and Energy 2021 Forum, 3586, 2021 | 7 | 2021 |
Dual-bell nozzle with fluidic control of transition for space launchers A Ferrero, A Conte, E Martelli, F Nasuti, D Pastrone Acta Astronautica 193, 130-137, 2022 | 6 | 2022 |
Numerical tool optimization for advanced rocket nozzle performance prediction A Conte, A Ferrero, F Larocca, D Pastrone AIAA Propulsion and Energy 2019 Forum, 4115, 2019 | 6 | 2019 |
Numerical investigation for performance prediction of gas dynamic resonant igniters A Conte, A Ferrero, D Pastrone Advances in aircraft and spacecraft science 7 (5), 425-440, 2020 | 4 | 2020 |
Preliminary study of a resonant igniter for rocket engines A Conte, A Ferrero, D Pastrone AIP Conference Proceedings 2293 (1), 2020 | 2 | 2020 |
Thermal analysis of a hybrid rocket propulsion system for interplanetary cubesats S Contadin, A Conte, AC Karp, ET Jens, D Vaughan, DG Pastrone 7TH European Conference for Aeronautics and Aerospace Sciences (EUCASS), 2017 | 2 | 2017 |
Simple, affordable evaporative cooler to reduce food loss in developing countries F Collarin, A Conte, F Marasca, L Mascolo, L Massa, F Mutti, MT Sposato CERN IdeaSquare Journal of Experimental Innovation 3 (2), 18-22, 2019 | 1 | 2019 |
CFD Simulation of Hybrid Rocket Motors for Interplanetary CubeSats A Conte, S Contadin, AC Karp, ET Jens, D Vaughan, DG Pastrone 7TH European Conference for Aeronautics and Aerospace Sciences (EUCASS), 2017 | 1 | 2017 |
Experimental investigation of the effects of different internal surface features on additive-manufactured resonant igniters performance A Conte, G Gedda, S Lerda, F Masseni, S Biamino, A Ferrero, ... Acta Astronautica 218, 290-297, 2024 | | 2024 |
SmallSat hybrid propulsion system AC Karp, E Jens, J Rabinovitch, B Nakazono, A Conte US Patent 11,578,682, 2023 | | 2023 |
Advanced Concepts for Rocket Engine Applications A Conte Politecnico di Torino, 2022 | | 2022 |
Parametric study of transition fluidic control in a dual-bell nozzle A Ferrero, A Conte, E Martelli, F Nasuti, D Pastrone, V Roma 9ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS), 2022 | | 2022 |
Europa Lander Plume-Induced Contamination: DSMC Modeling of Monopropellant Plume Testing A Conte, WA Hoey, A Wong, CE Soares, M Grabe, C Hepp | | 2021 |
Design, Modeling and Testing of a O2/CH4 Igniter for a Hybrid Rocket Motor D Vaughan, B Nakazono, AC Karp, E Jens, J Rabinovich, A Conte Pasadena, CA: Jet Propulsion Laboratory, National Aeronautics and Space …, 2018 | | 2018 |
CFD analysis of hybrid rocket motors for interplanetary CubeSats D Pastrone, D Vaughan, E Jens, AC Karp, S Contadin, A Conte Pasadena, CA: Jet Propulsion Laboratory, National Aeronautics and Space …, 2017 | | 2017 |