Title of article :
Reduced environmental impact by lowered cruise altitude for liquid hydrogen-fuelled aircraft
Author/Authors :
Svensson، نويسنده , , Fredrik and Hasselrot، نويسنده , , Anders and Moldanova، نويسنده , , Jana، نويسنده ,
Issue Information :
روزنامه با شماره پیاپی سال 2004
Abstract :
Environmental concerns, as well as the expected depletion of fossil fuel resources, have become the driving forces for research and development towards the introduction of hydrogen energy into air traffic. The present paper is a summary of a study that was carried out within the European sponsored project CRYOPLANE, co-ordinated by Airbus Germany.
jectives of this study are to re-optimise and compare two equivalent medium-range aircraft – one kerosene-fuelled and one LH2-fuelled – for reduced cruise altitude, from an environmental point of view. By lowering the cruise altitude, the contribution to global warming might be reduced at the expense of increased fuel consumption and pollutant emissions.
er to assess the global impact, in terms of global warming, from the emissions discharged on a certain mission, a simple parametric model is employed.
sults suggest that introduction of cryoplanes will improve the environmental performance, particularly in terms of global warming. Provided that an increase in fuel consumption in the order of 10% and an increase in TOM of a few percent are accepted, the results suggest that cryoplanes should cruise at an altitude of about 2–3 km below where conventional aircraft cruise today in order to considerably reduce the environmental impact.
Keywords :
Optimisation , Environmental impact , aircraft performance , GLOBAL WARMING , Marschhِjd , Optimering , Miljِpهverkan , Flygplanprestanda , Global uppvنrmning , Cruise altitude
Journal title :
Aerospace Science and Technology
Journal title :
Aerospace Science and Technology