Overview of the Clean Sky 2 Technology Evaluator Project Methodology †
Abstract
:1. Introduction
- Increase aircraft fuel efficiency, thus reducing CO2 emissions by from 20% to 30% compared to “state-of-the-art” aircraft entering service from 2014.
- Reduce aircraft NOx and noise emissions by from 20 to 30% compared to “state-of-the-art” aircraft entering service from 2014 [1].
- The five aviation normative scenarios from ATAG, which were part of the “Waypoint 2050” study, represent global outlooks of emission reductions in aviation under different assumptions [4].
- The global “Net Zero Carbon 2050 Resolution” from IATA is also a normative scenario study, which includes market-based measures for emissions reduction [5].
- The “Long-term Global Aspirational Goal (LTAG)” for international aviation of net-zero carbon emissions by 2050, set by ICAO, which, however, does not attribute specific obligations or commitments in the form of emissions reduction goals to individual states [6].
- The “ACARE Vision” for net-zero CO2 emissions for all intra-EU flights and those departing the EU [7].
- “Flightpath 2050” is a vision for a leading European aviation industry that is clean, competitive, sustainable, safe and secure [8].
2. Methods: Structure and Methodology of the Technology Evaluator Within the Clean Sky 2 Program
- Large passenger aircraft: within this platform, an advanced short–medium-range (SMR) aircraft shows the potential of ultra-high bypass ratio engines (UHBRs), complemented by an ultra-advanced SMR dealing mainly with open fan engines and additionally an advanced long-range aircraft covering the potential of ultra-fan engines.
- Regional aircraft: this platform covers a 70-seat multi-mission turboprop aircraft and a 90-seat and 130-seat turboprop passenger aircraft.
- Fast Rotorcraft: this platform includes two fast rotorcraft configurations, the Next Generation Civil Tilt Rotor (NGCTR) and a compound configuration (Rapid and Cost-Effective Rotorcraft, RACER).
- An aircraft performance module that calculates the trajectory of a given mission for the aircraft.
- An emissions module that calculates the Emissions (CO2 and NOx) along the trajectory of a given mission for the aircraft.
- A noise module that calculates the noise on the ground through noise hemispheres at the take-off and landing phases of the aircraft.
- Airport simulation: This comprises specific data on airport and airspace layout (infrastructure and the various airspace control areas) for each airport; airport and airspace operations, e.g., flight procedures and rules, including the way aircraft are handled at the ground and in the air by the airport and air-traffic control. It also takes into account the maximum number of aircraft movements that an airport can handle as opposed to an unconstrained forecast.
- Noise calculation: Based on aircraft performance characteristics from the mission level aircraft models and specific airport traffic scenarios coming from the ATS level, Lden and Lnight noise contours and noise expressed in terms of the SEL (Sound Exposure Level) are calculated.
- Emission calculation: Based on aircraft performance characteristics from the mission level aircraft models and specific airport traffic scenarios coming from the ATS level, the amount of CO2 and NOX in kg emitted during a flight below 3000 ft by aircraft is calculated.
- Lden: Cumulative noise level (in dB(A)) over an entire year for multiple events, with a penalty for aircraft operations during evening- and night-time
- Lnight: Cumulative noise level (in dB(A)) over an entire year for aircraft operations during night-time.
- A “Constrained Scenario”, which considers future capacity constraints at the airports globally.
- An “Unconstrained Scenario”, which does not include future capacity constraints at airports and is comparable to established forecasts like those of Airbus, Boeing, ICAO and IATA.
- A “SAF Scenario”, which considers the introduction of sustainable aviation fuels in future fleets according to ReFuel EU on a global level.
- A “Constrained People Mover Scenario”, where, additionally to the inclusion of the Clean Sky 2 concept aircraft from the industrial partners, the People Mover is introduced from 2034 into the fleet. The People Mover is a large 580-seat aircraft that has been designed for short- to medium-haul missions up to 4000 km.
- Forecast of passenger and flight demand the scenarios up to 2050.
- Determination of the fleet mix of future fleets up to 2050 including the Entry into Service of future concept aircraft coming from the mission-level aircraft models leading to a flight plan of the whole fleet with all airport pairs globally.
- Emission inventory calculation for the global fleet for all airport pairs.
3. Results: Technology Evaluator Assessment Framework and Metrics
4. Discussion and Conclusions
Author Contributions
Funding
Data Availability Statement
Conflicts of Interest
Abbreviations
ACARE | Advisory Council for Aeronautics Research in Europe |
AIR | Clean Sky 2 Airframe ITD |
ATAG | Air Transport Action Group |
ATS | Air transport system |
EASA | European Aviation Safety Agency |
IADP | Innovative Aircraft Demonstrator Platforms |
ITD | Integrated Technology Demonstrators |
IATA | International Air Transport Association |
ICAO | International Civil Aviation Organization |
CAGR | Compound annual growth rate |
CO2 | Carbon dioxide |
CS2 | Clean Sky 2 |
dB(A) | Decibels on the A scale |
DLR | Deutsches Zentrum für Luft- und Raumfahrt e.V. (German Aerospace Center) |
DLR CON | DLR constrained forecast |
DLR UC | DLR unconstrained forecast |
ENG | Clean Sky 2 Engine ITD |
E-STOL | Electrical/hybrid short take-off and landing aircraft concept |
EU | European Union |
FRC | Clean Sky 2 Fast RotorCraft IADP |
GDP | Gross domestic product |
GTF | Geared turbofan |
ft | Feet |
kft | Kilo-feet |
kTAS | Knots true air speed |
LAQ | Local air quality |
Lden | Cumulative noise level (in dB(A)) over an entire year for multiple events, with a penalty for aircraft operations during evening- and night-time |
Lnight | Cumulative noise level (in dB(A)) over an entire year for aircraft operations during night-time. |
LPA | Clean Sky 2 Large Passenger Aircraft IADP |
LTAG | Long-term Global Aspirational Goal |
Ma | Mach number |
NB | Narrowbody |
NGCTR | Next Generation Civil Tilt Rotor |
NOx | Nitrogen oxides |
RACER | Rapid and Cost-Effective Rotorcraft |
REG | Clean Sky 2 Regional IADP |
RPK | Revenue passenger kilometres |
SAF | Sustainable aviation fuel |
SAT | Small Air Transport |
SEL | Sound exposure level |
SID | Standard Instrument Departures |
SMR | Short-medium-range |
SoA | State-of-art |
STAR | Standard Terminal Arrival Routes |
TA | Transverse Activities |
TE | Technology Evaluator |
TP | Turboprop |
UHBR | Ultra-high bypass ratio |
UK | United Kingdom |
WB | Widebody |
# | Number |
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Junior, A.; Leipold, A.; Gelhausen, M.C. Overview of the Clean Sky 2 Technology Evaluator Project Methodology. Aerospace 2025, 12, 268. https://doi.org/10.3390/aerospace12040268
Junior A, Leipold A, Gelhausen MC. Overview of the Clean Sky 2 Technology Evaluator Project Methodology. Aerospace. 2025; 12(4):268. https://doi.org/10.3390/aerospace12040268
Chicago/Turabian StyleJunior, Alf, Alexandra Leipold, and Marc C. Gelhausen. 2025. "Overview of the Clean Sky 2 Technology Evaluator Project Methodology" Aerospace 12, no. 4: 268. https://doi.org/10.3390/aerospace12040268
APA StyleJunior, A., Leipold, A., & Gelhausen, M. C. (2025). Overview of the Clean Sky 2 Technology Evaluator Project Methodology. Aerospace, 12(4), 268. https://doi.org/10.3390/aerospace12040268