MDO and REgulations for Low-boom and Environmentally Sustainable Supersonic aviation

Project Information

MOREandLESS

Grant agreement ID: 101006856

DOI 10.3030/101006856

EC signature date 6 November 2020

Start date 1 January 2021

End date 31 December 2024

Funded under

• SOCIETAL CHALLENGES - Smart, Green And Integrated Transport

Total cost € 6 336 211,25

EU contribution € 4 999 996,25

Coordinated by

POLITECNICO DI TORINO
Italy

Deliverables

Documents, reports (8)

Project Exploitation Plan

This deliverable enumerates and analyses possible strategies for the utilisation of results in further research activities other than those covered by the present research project or in developing creating and marketing a product or process or in creating and providing a service or in standardisation activities This deliverable is related to Task 13

Comparison between EU and US current Regulatory Framework. Interim Report

The deliverable contains the results of the comparison analysis between EU and US current regulatory framework Guidelines for a common vision are also included This deliverable is related to Tasks 731 and 732

Current regulatory framework for supersonic aviation

The deliverable collects the results of the analysis of the current regulatory framework focusing on emissions for air quality and climate impact and on noise for LTO cycles and sonic boom for supersonic aviation and it is related to Task 71

Modelling set-up for air quality, atmospheric impact and climate, including a description of the aviation emission scenarios

This Deliverable collects results achieved in modelling setup for air qualityatmospheric impact and climate including a description of the aviation emission scenarios inventories This deliverable relates to Task 51

Sonic boom generation (impact of vehicle configuration) and evaluation based on RANS CFD simulations

This deliverable collects the results of aerodynamics simulations of reference aircraft to determine the sonic boom generation and nearfield flow pattern This deliverable relates to Task 351

CS-0 and CS-2 Case Studies Definition

This deliverable collects the results of CS0 and CS2 casestudies definition including the preliminary assessment of subsonic reference aircraft Task 211 Task 212 and Task 213 and CS2 Task 231

Suggestions for potential future directions for the regulatory framework: identifying priority work items and rationale. First interim report

The deliverable contains suggestions for potential future directions for the regulatory framework that has to be updated every 12 months following CAEP cycles This deliverable is related to Task 71

Requirements for human participation

This deliverable is completed according to the ethics selfassessment procedure suggested for H2020 Projects This deliverable is related to Task 12

Websites, patent fillings, videos etc. (1)

Project Website and social network project profiles

This deliverable consists in a guide for users and developers of the Project Website In addition once the official social network is selected and the project profile is created a short guide to login and update the profile is added This deliverable is related to Task 12

Publications

Peer reviewed articles (2)

Sensitivities of atmospheric composition and climate to altitude and latitude of hypersonic aircraft emissions

Author(s): Johannes Friedrich Pletzer and Volker Grewe
Published in: Atmos. Chem. Phys., 2023, ISSN 1680-7316
Publisher: European Geophysical Society
DOI: 10.5194/egusphere-2023-1777

The Climate Impact of Hypersonic Transport

Author(s): Pletzer J., Hauglustaine, D., Cohen, Y., Jöckel, P., and Grewe, V.
Published in: Atmos. Chem. Phys., 2022, ISSN 1680-7316
Publisher: European Geophysical Society
DOI: 10.5194/egusphere-2022-285

Conference proceedings (5)

Aerodatabase development and integrationn of supersonic/hypersonic cruiser vehicles in MORE&LESS Project

Author(s): P. Roncioni, M. Marini, R. Fusaro, N. Viola
Published in: Proceedings of the 33rd Congress of the International Council of the Aeronautical Sciences, Issue 4-9 September 2022, 2022
Publisher: ICAS

Simplified models for the preliminary aerodynamic characterization of high-speed vehicles to support mission analysis

Author(s): O. Gori
Published in: Proceedings of the 33rd Congress of the International Council of the Aeronautical Sciences, Issue 4-9 September 2022, 2022
Publisher: ICAS

LTO noise and sonic boom predictions in early conceptual design phases

Author(s): G. Piccirillo, S. Graziani, R. Fusaro, N. Viola
Published in: Proceedings of the 33rd Congress of the International Council of the Aeronautical Sciences, Issue 4-9 September 2022, 2022
Publisher: ICAS

Hypersonic aircraft and mission concept re-design to move from Mach 8 to Mach 5 operations

Author(s): N. Viola, R. Fusaro, D. Ferretto, O. Gori, M. Marini, P. Roncioni, B.O. Cakir, A.C. Ispir, B.H. Saracoglu
Published in: Proceedings of the 33rd Congress of the International Council of the Aeronautical Sciences, Issue 4-9 September 2022, 2022
Publisher: ICAS

High pressure hydrogen oxygen combustion kinetic assessment for air-breathing propulsion supersonic green aviation

Author(s): G.Saccone, M. Marini
Published in: Proceedings of the 33rd Congress of the International Council of the Aeronautical Sciences, Issue 4-9 September 2022, 2022
Publisher: ICAS