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TRIMIS

Stratospheric Flying Opportunities for High-Speed Propulsion Concepts

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete
Geo-spatial type
Other
Total project cost
€4 000 000
EU Contribution
€4 000 000
Project website
Project Acronym
STRATOFLY
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Societal/Economic issues,
Safety/Security,
Digitalisation
Transport sectors
Passenger transport,
Freight transport

Overview

Link to CORDIS
Background & Policy context

The stratosphere is the highest layer in the atmosphere where aircraft can still fly. Nevertheless, it is presently rarely exploited for commercial aviation. As Europe’s Vision for Aviation predicts globally a six-fold increase in passenger by 2050, flight levels above the troposphere become attractive and maybe the only way to realize this.

While the lower stratosphere could still be reachable for classical aircraft, the higher altitudes would demand for higher speeds. Various technologies, systems and novel aircraft concepts related to high-speed transport have progressed rapidly over the last 20 years showing their technical feasibility and readiness up to TRL-3. Technology roadmaps elaborated by industrial and research teams indicated their readiness-level can easily be brought up to TRL-6 by 2035 provided the related application can be shown to be commercially exploitable.

Objectives

The first project goal covers the multi-functional integration of propulsion, aerodynamics, airframes and on-board systems across various disciplines to define and detail a high-speed aircraft configuration enabling long-haul travels.

However, Europe should have simultaneously a directive which flight altitudes are environmentally sustainable on the basis of fuel type and emission rates. This parametric mapping of the stratospheric climate impact covers the second goal of the project.

Last but not least, the potential of stratospheric flight relies also on economic viability. Apart from potential routes, aircraft capacity and performance, development and exploitation costs… the third goal will also consider human factors, social acceptance, implementation and noise issues.

The present proposal will, contrary to regular viability studies, perform a bottom-up approach. The validity will follow a sound technical and scientific approach and shall demonstrate environmental and economic compatibility. This enables then a formulation of regulatory, technological and socio-economic barriers.

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
European Commission
Type of funding
Public (EU)
Specific funding programme
H2020-EU.3.4.
Other Programme
MG-1-4-2016-2017 Breakthrough innovation

Partners

Lead Organisation
Organisation
Politecnico Di Torino
Address
Corso Duca Degli Abruzzi, 10129 Torino, Italy
Organisation website
EU Contribution
€375 000
Partner Organisations
Organisation
Totalforsvarets Forskningsinstitut
Address
Gullfossgatan, 164 90 Stockholm, Sweden
Organisation website
EU Contribution
€270 000
Organisation
Stichting Centrum Voor De Ontwikkeling Van Transport En Logistiek In Europa
Address
Van Nelleweg 1, 3044 BC Rotterdam, Netherlands
Organisation website
EU Contribution
€325 000
Organisation
Technische Universitat Hamburg
Address
Am Schwarzenberg Campus 1, 21073 Hamburg, Germany
Organisation website
EU Contribution
€400 000
Organisation
Office National D' Etudes Et De Recherches Aérospatiales
Address
29, avenue de la Division Leclerc, BP72 CHÂTILLON CEDEX, France
Organisation website
EU Contribution
€350 000
Organisation
Deutsches Zentrum Fr Luft Und Raumfahrt E.v
Address
Linder Hoehe, 51147 KOELN, Germany
Organisation website
EU Contribution
€650 000
Organisation
Fundacion De La Ingenieria Civil De Galicia
Address
Escuela Ingenieros De Caminos/universidad De Coruna/campus De Elvina, 15071 La Coruna, Spain
EU Contribution
€315 000
Organisation
Centro Italiano Ricerche Aerospaziali Scpa
Address
Via Maiorise s/n, 81043 CAPUA (CE), Italy
Organisation website
EU Contribution
€515 000
Organisation
Institut Von Karman De Dynamique Des Fluides
Address
Chaussee De Waterloo 72, 1640 Rhode Saint Genese, Belgium
EU Contribution
€600 000
Organisation
Centre National De La Recherche Scientifique
Address
3 rue Michel-Ange, 75794 PARIS, France
Organisation website
EU Contribution
€200 000

Technologies

Technology Theme
Aircraft design and manufacturing
Technology
Suborbital point to point aircraft
Development phase
Research/Invention

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