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Dr. Antonietta Conte
Titel
Zitiert von
Zitiert von
Jahr
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
282018
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
192018
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
132018
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
92017
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
72021
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
52019
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
42022
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
42020
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
22017
Preliminary study of a resonant igniter for rocket engines
A Conte, A Ferrero, D Pastrone
AIP Conference Proceedings 2293 (1), 2020
12020
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
12019
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
12017
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, 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
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