A space aircraft including a fuselage, two wings arranged on either side of the fuselage, and two nacelles arranged at the ends of the wings and each carrying a horizontal tail and a vertical tail, the fuselage having a cross section of variable size along the longitudinal axis with a maximum cross section being located in a longitudinal position located in front of the longitudinal position of the leading edges of the wings at the fuselage, making it possible in particular to help prevent the space aircraft from losing longitudinal static stability, the space aircraft thus having an optimized design and architecture which are suitable for the severe conditions encountered by such a space aircraft, in particular during atmospheric re-entry.


    Access

    Download


    Export, share and cite



    Title :

    SPACE AIRCRAFT WITH OPTIMISED DESIGN AND ARCHITECTURE


    Contributors:

    Publication date :

    2022-10-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    Power-Optimised Aircraft

    Rothammer, W. / Hamburg Messe und Congress GmbH | British Library Conference Proceedings | 2004


    Optimised aircraft cabin layout

    SAINT-JALMES BRUNO / ZANEBONI JASON / RUMEAU BERNARD | European Patent Office | 2015

    Free access

    Optimised lighting systems architecture

    Dubrovin, A. | Tema Archive | 2001


    Optimised Lighting Systems Architecture

    Dubrovin, A. | British Library Conference Proceedings | 2001


    DOUBLE-CURVED AIRCRAFT DOOR WITH OPTIMISED LOCKING MEANS

    DEVILLEZ SÉBASTIEN / DUCASSE JEAN FRANCOIS | European Patent Office | 2023

    Free access