David Victor Azzaro Bradea
Preliminary assessment of a liquid methane powered commercial hypersonic aircraft.
Rel. Davide Ferretto, Roberta Fusaro. Politecnico di Torino, Master of science program in Aerospace Engineering, 2025
|
Preview |
PDF (Tesi_di_laurea)
- Thesis
Licence: Creative Commons Attribution Non-commercial No Derivatives. Download (7MB) | Preview |
|
|
Archive (ZIP) (Documenti_allegati)
- Other
Licence: Creative Commons Attribution Non-commercial No Derivatives. Download (39kB) |
Abstract
In the early 1970s, different studies related to the potential exploitation of liquid methane as fuel for long range supersonic and hypersonic commercial aircraft were carried out in the US, in order to verify the competitiveness of an alternative vehicle architecture which could compete against the European Concorde. In the end, the studies did not produce a concrete vehicle concept, but the theoretical foundations of the studies are still valid nowadays. On the other hand, the wide interest in hydrogen for aviation produced, more recently, different concepts and studies, also in the field of high-speed aviation, however often highlighting the limitations related to storage capabilities and thermal management.
Liquid methane, can offer higher energy per unit mass with reference to kerosene, benefitting from only half the density and producing thus an advantage with reference to hydrogen from the point of view of energy per unit volume
Relators
Academic year
Publication type
Number of Pages
Course of studies
Classe di laurea
URI
![]() |
Modify record (reserved for operators) |
