CONTE, ANTONIETTA

CONTE, ANTONIETTA  

Dipartimento di Ingegneria Meccanica e Aerospaziale  

042528  

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Risultati 1 - 15 di 15 (tempo di esecuzione: 0.012 secondi).
Citazione Data di pubblicazione Autori File
Experimental investigation of the effects of different internal surface features on additive-manufactured resonant igniters performance / Conte, Antonietta; Gedda, Giacomo; Lerda, Serena; Masseni, Filippo; Biamino, Sara; Ferrero, Andrea; Marchese, Giulio; Pastrone, Dario. - In: ACTA ASTRONAUTICA. - ISSN 0094-5765. - (2024). [10.1016/j.actaastro.2024.02.043] 1-gen-2024 Conte, AntoniettaGedda, GiacomoLerda, SerenaMasseni, FilippoBiamino, SaraFerrero, AndreaMarchese, GiulioPastrone, Dario 1-s2.0-S0094576524001152-main.pdf
Advanced Concepts for Rocket Engine Applications / Conte, Antonietta. - (2022 Apr 13), pp. 1-179. 13-apr-2022 CONTE, ANTONIETTA conv_dissertation_aconte.pdfconv_summary_aconte.pdf
Dual-bell nozzle with fluidic control of transition for space launchers / Ferrero, Andrea; Conte, Antonietta; Martelli, Emanuele; Nasuti, Francesco; Pastrone, Dario. - In: ACTA ASTRONAUTICA. - ISSN 0094-5765. - STAMPA. - 193:(2022), pp. 130-137. [10.1016/j.actaastro.2021.12.048] 1-gen-2022 Andrea FerreroAntonietta ConteEmanuele MartelliDario Pastrone + paper-postprint.pdfpreprint.pdf1-s2.0-S0094576521006949-main.pdf
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
Numerical investigation for performance prediction of gas dynamic resonant igniters / Conte, Antonietta; Ferrero, Andrea; Pastrone, Dario Giuseppe. - In: ADVANCES IN AIRCRAFT AND SPACECRAFT SCIENCE. - ISSN 2287-528X. - 7:5(2020), pp. 425-440. [10.12989/aas.2020.7.5.425] 1-gen-2020 Antonietta ConteFerrero AndreaDario Pastrone aas0705004.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.pdfresonant_igniter.pdf
SmallSat Hybrid Propulsion System / C. Karp, Ashley; Jens, Elizabeth; Rabinovitch, Jason; Nakazono, Barry; Conte, Antonietta. - (2020). 1-gen-2020 Antonietta, Conte + -
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
Simple, affordable evaporative cooler to reduce food loss in developing countries / Collarin, F.; Conte, A.; Marasca, F.; Mascolo, L.; Massa, L.; Mutti, F.; Sposato, M. T.. - In: CERN IDEASQUARE JOURNAL OF EXPERIMENTAL INNOVATION. - ISSN 2413-9505. - ELETTRONICO. - 3:2(2019), pp. 18-22. [10.23726/cij.2019.881] 1-gen-2019 A. ConteL. Mascolo + 881-4145-2-PB.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 + -