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In this paper, the activities at the German Aerospace Center (DLR) related to the conceptual design studies of aircraft configurations with hybrid electric propulsion for a typical short range commercial transport mission in the scope of the European Clean Sky 2 program in the project "Advanced Engine and Aircraft Configurations" (ADEC) are described. The configurations analyzed incorporate different hybrid powertrain architectures consisting of gas turbines, electric machines, and batteries. Technologies as distributed propulsion are utilized for the boundary layer ingestion at the fuselage and for the powered yaw control. The synergetic effects of a canard configuration and a BLI propulsor at the rear of the fuselage are investigated. The focus of this paper is on the quantitative evaluation of configurations utilizing a conceptual aircraft sizing workflow built in the DLR's "Remote Component Environment" incorporating semi-empirical and low level physics based methods. In order to depict the rationale behind the investigated aircraft configurations, a brief overview of the foregone downselection process is given. The concepts evaluated in the scope of this work are shown. The multi-disciplinary overall aircraft sizing workflow is described. An overview of reference configurations is given. The design space studies of configurations with hybrid electric propulsion are presented. The most promising configurations are shown in detail and compared to the advanced reference aircraft. Finally, a conclusion is drawn and an outlook is presented. This project has received funding from the Clean Sky 2 Joint Undertaking (JU) under grant agreement No 807097 . The JU receives support from the European Union's Horizon 2020 research and innovation programme and the Clean Sky 2 JU members other than the Union. The results, opinions, conclusions, etc. presented in this work are those of the author(s) only and do not necessarily represent the position of the JU; the JU is not responsible for any use made of the information ...

Although about two-thirds of aviation's climate impacts are caused by non-CO2 effects, such as ozone production or contrail cirrus formation, these effects are not yet considered in existing and currently planned policy instruments (e.g. EU ETS or CORSIA). Due to their climatological relevance, however, various economic concepts have been proposed recently to internalise nonCO2 effects. Most of these approaches are based on the principle of equivalent CO2 emissions (CO2e), a way of unitizing the impact of all climate agents. Several calculation methods for CO2 equivalents are in principle available, which differ in the degree of detail and are subject to uncertainties related to atmospheric science. There are a quite a few key decision parameters for policy makers for setting up a monitoring, reporting, and verification (MRV) scheme for non-CO2 effects. The aim of this study is therefore to analyze and discuss the most important decision parameters for the integration of non-CO2 aviation effects into EU ETS.

In addition to carbon dioxide, air traffic operation affects the climate through other emissions and atmospheric processes, such as the formation of ozone and contrail cirrus. The climate impact of these non-CO2 effects is strongly dependent on the emission location (in particular cruise altitude) and emission time (e.g. weather conditions) and, thus, highly non-linear to the fuel consumption. Although non-CO2 effects are responsible for about 2/3 of the climate impact of aviation, they are not yet taken into account in existing and currently planned emissions trading systems (e.g. EU ETS) or market-based measures (MBM, e.g. CORSIA 1). This research project focuses on the development of concepts for the integration of non-CO2 effects of air traffic into the EU ETS and under CORSIA. For this purpose, suitable climate metrics for assessing the relationship between non-CO2 and CO2 climate impacts are analyzed first (Part A). For selected non-CO2 calculation methodologies, the availability of the necessary data is examined and estimation procedures for non-existent data are investigated (Part B). Afterwards, the current practice in voluntary carbon markets for estimating CO2 and non-CO2 effects of aviation is presented (Part C). The additional administrative burden to verify reporting on aviation's non-CO2 is examined in Part D. In the final step, key design parameters for the integration of non-CO2 consequences of aviation in the EU ETS and CORSIA are evaluated (Part E). The inclusion of non-CO2 effects in the EU ETS and CORSIA is highly recommended for climatelogical reasons and technically feasible, but involves an additional administrative burden for authorities and aircraft operators. The level of the resulting mitigation incentive as well as the additional effort is strongly depending on the calculation methodology of the CO2 equivalents. For this choice, a trade-off must be made between a simple operational feasibility and a high incentive level to modify flight routing and to reduce the NOx emission indices. False mitigation incentives, which can arise from to the non-linearity between non-CO2 climate effects and fuel consumption, must be prevented.

This paper describes the current activities at the German Aerospace Center (DLR) and an associated consortium related to conceptual design studies of an aircraft configuration with hybrid electric propulsion for a typical short range commercial transport mission. The work is implemented in the scope of the European Clean Sky 2 program in the project "Advanced Engine and Aircraft Configurations" (ADEC) and "Turbo electric Aircraft Design Environment" (TRADE). The configuration analyzed incorporates parallel hybrid architecture consisting of gas turbines, electric machines, and batteries that adds electric power to the fans of the engines. A conceptual aircraft sizing workflow built in the DLR's "Remote Component Environment" (RCE) incorporating tools of DLR that are based on semi-empirical and low level physics based methods. The TRADE consortium developed a simulation and optimization design platform with analysis models of higher fidelity for an aircraft with hybrid electric propulsion architecture. An implementation of the TRADE simulation and optimization design platform into the DLR's RCE workflow by replacing the DLR models was carried out. The focus of this paper is on the quantitative evaluation of the "Boosted Turbofan" configuration utilizing the resulting workflow. In order to understand the cooperation between the DLR and TRADE consortium, a brief overview of the activities is given. Then the multi-disciplinary overall aircraft sizing workflow for hybrid electric aircraft built in RCE is shown. Hereafter, the simulation and optimization models of the TRADE design platform are described. Subsequently, an overview of the aircraft configurations considered in the scope of this work is given. The design space studies of the "Boosted Turbofan" configuration are presented. Finally, the deviations of the results between the workflows with and without the TRADE modules are discussed. This project has received funding from the Clean Sky 2 Joint Undertaking (JU) under grant agreement No 807097 . The JU receives ...