Archivio Istituzionale della RicercaCONTE, ANTONIETTA
CONTE, ANTONIETTA
Dipartimento di Ingegneria Meccanica e Aerospaziale
042528
Dual-bell nozzle for space launchers with fluidic control of transition
2021 Ferrero, A.; Conte, A.; Martelli, E.; Nasuti, F.; Pastrone, D.
Preliminary study of a resonant igniter for Rocket Engines
2020 Conte, Antonietta; Ferrero, Andrea; Pastrone, Dario Giuseppe
Numerical Tool Optimization for Advanced Rocket Nozzle Performance Prediction
2019 Conte, Antonietta; Ferrero, Andrea; Larocca, Francesco; Pastrone, Dario Giuseppe
Characterization of PolyMethylMethAcrylate as a Fuel for Hybrid Rocket Motors
2018 Rabinovitch, Jason; Jens, Elizabeth T.; Karp, Ashley C.; Nakazono, Barry; Conte, Antonietta; Vaughan, David A.
Design of Interplanetary Hybrid CubeSat and SmallSat Propulsion Systems
2018 Jens, Elizabeth T.; Karp, Ashley C.; Rabinovitch, Jason; Conte, Antonietta; Nakazono, Barry; Vaughan, David A.
Design, modeling and testing of a O2/CH4 igniter for a hybrid rocket motor
2018 Conte, Antonietta; Rabinovitch, Jason; Jens, Elizabeth; Karp, Ashley Chandler; Nakazono, Barry; Vaughan, David A.
CFD Simulation of Hybrid Rocket Motors for Interplanetary CubeSats
2017 Conte, Antonietta; Contadin, Stefania; Ashley, Karp; Elizabeth, Jens; David, Vaughan; Pastrone, Dario Giuseppe
Development Testing of Hybrid Rocket Motors Using Classical Fuels for Interplanetary CubeSats
2017 Jens, Elizabeth T.; Karp, Ashley C.; Contadin, Stefania; Conte, Antonietta; Nakazono, Barry; Vaughan, David
Thermal Analysis of a Hybrid Rocket Propulsion System for Interplanetary CubeSats
2017 Contadin, Stefania; Conte, Antonietta; Karp, Ashley; Jens, Elizabeth; Vaughan, David; Pastrone, Dario Giuseppe
| Citazione | Data di pubblicazione | Autori | File |
|---|---|---|---|
| Dual-bell nozzle for space launchers with fluidic control of transition / Ferrero, A.; Conte, A.; Martelli, E.; Nasuti, F.; Pastrone, D.. - ELETTRONICO. - (2021), pp. 1-9. (Intervento presentato al convegno AIAA Propulsion and Energy 2021 Forum tenutosi a VIRTUAL EVENT nel August 9-11, 2021). | 1-gen-2021 | Ferrero A.Conte A.Martelli E.Pastrone D. + | paper.pdf |
| Preliminary study of a resonant igniter for Rocket Engines / Conte, Antonietta; Ferrero, Andrea; Pastrone, Dario Giuseppe. - ELETTRONICO. - (2020). (Intervento presentato al convegno 17th International Conference of Numerical Analysis and Applied Mathematics ICNAAM 2019 tenutosi a Rhodes, Greece nel 23-28 September 2019) [10.1063/5.0026699]. | 1-gen-2020 | Antonietta ConteAndrea FerreroDario Pastrone | 5.00266993.pdf; resonant_igniter.pdf |
| Numerical Tool Optimization for Advanced Rocket Nozzle Performance Prediction / Conte, Antonietta; Ferrero, Andrea; Larocca, Francesco; Pastrone, Dario Giuseppe. - ELETTRONICO. - (2019). (Intervento presentato al convegno AIAA Propulsion and Energy 2019 Forum tenutosi a Indianapolis (USA) nel 19-22 August 2019) [10.2514/6.2019-4115]. | 1-gen-2019 | Antonietta ConteAndrea FerreroFrancesco LaroccaDario Pastrone | dual_bell_indianapolis2019.pdf |
| Characterization of PolyMethylMethAcrylate as a Fuel for Hybrid Rocket Motors / Rabinovitch, Jason; Jens, Elizabeth T.; Karp, Ashley C.; Nakazono, Barry; Conte, Antonietta; Vaughan, David A.. - (2018). (Intervento presentato al convegno 2018 Joint Propulsion Conference tenutosi a Cincinnati, Ohio (USA)) [10.2514/6.2018-4530]. | 1-gen-2018 | Conte, Antonietta + | - |
| Design of Interplanetary Hybrid CubeSat and SmallSat Propulsion Systems / Jens, Elizabeth T.; Karp, Ashley C.; Rabinovitch, Jason; Conte, Antonietta; Nakazono, Barry; Vaughan, David A.. - ELETTRONICO. - (2018). (Intervento presentato al convegno 2018 Joint Propulsion Conference tenutosi a Cincinnati, Ohio (USA)) [10.2514/6.2018-4668]. | 1-gen-2018 | Conte, Antonietta + | - |
| Design, modeling and testing of a O2/CH4 igniter for a hybrid rocket motor / Conte, Antonietta; Rabinovitch, Jason; Jens, Elizabeth; Karp, Ashley Chandler; Nakazono, Barry; Vaughan, David A.. - ELETTRONICO. - (2018). (Intervento presentato al convegno 48th AIAA Fluid Dynamics Conference, 2018 tenutosi a usa nel 2018) [10.2514/6.2018-3239]. | 1-gen-2018 | Conte, Antonietta + | - |
| CFD Simulation of Hybrid Rocket Motors for Interplanetary CubeSats / Conte, Antonietta; Contadin, Stefania; Ashley, Karp; Elizabeth, Jens; David, Vaughan; Pastrone, Dario Giuseppe. - ELETTRONICO. - (2017). (Intervento presentato al convegno 7TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS)) [10.13009/eucass2017-614]. | 1-gen-2017 | CONTE, ANTONIETTACONTADIN, STEFANIADario PASTRONE + | - |
| Development Testing of Hybrid Rocket Motors Using Classical Fuels for Interplanetary CubeSats / Jens, Elizabeth T.; Karp, Ashley C.; Contadin, Stefania; Conte, Antonietta; Nakazono, Barry; Vaughan, David. - (2017). (Intervento presentato al convegno 53rd AIAA/SAE/ASEE Joint Propulsion Conference tenutosi a Atlanta, GA (USA)) [10.2514/6.2017-4981]. | 1-gen-2017 | Conte, Antonietta + | - |
| Thermal Analysis of a Hybrid Rocket Propulsion System for Interplanetary CubeSats / Contadin, Stefania; Conte, Antonietta; Karp, Ashley; Jens, Elizabeth; Vaughan, David; Pastrone, Dario Giuseppe. - ELETTRONICO. - (2017). (Intervento presentato al convegno 7 TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS)) [10.13009/eucass2017-613]. | 1-gen-2017 | Stefania CONTADINAntonietta CONTEDario PASTRONE + | - |