The aim of this work is to promote the hypersonic flight in order to improve both the affordability of the access to space and the terrestrial flight transportation increasing flight range and reducing flight time. A strategic air vehicle is envisaged partially employing state-of-the-art technologies focusing on configuration and feasibility studies. The purpose is obviously to indicate the technologies on which concentrating the design efforts. To enable the development of future spacecraft, it is believed that the effort have to focused on the development, at low cost, of new technology demonstrator aircraft based on suborbital “tourism spacecraft” and fighter aircraft. An important goal would be the development of small and affordable aircraft able to perform the hypersonic cruise.

Hypothesis for Hypersonic Flight development / Chiesa, Sergio; CRESTO ALEINA, Sara; Fioriti, Marco; Fusaro, Roberta. - (2014). (Intervento presentato al convegno 1st International Symposium on “Hypersonic flight: from 100.000 to 400.000 ft” tenutosi a Rome (IT) nel 30 June - 1 July 2014).

Hypothesis for Hypersonic Flight development

CHIESA, Sergio;CRESTO ALEINA, SARA;FIORITI, MARCO;FUSARO, ROBERTA
2014

Abstract

The aim of this work is to promote the hypersonic flight in order to improve both the affordability of the access to space and the terrestrial flight transportation increasing flight range and reducing flight time. A strategic air vehicle is envisaged partially employing state-of-the-art technologies focusing on configuration and feasibility studies. The purpose is obviously to indicate the technologies on which concentrating the design efforts. To enable the development of future spacecraft, it is believed that the effort have to focused on the development, at low cost, of new technology demonstrator aircraft based on suborbital “tourism spacecraft” and fighter aircraft. An important goal would be the development of small and affordable aircraft able to perform the hypersonic cruise.
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11583/2628321
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