Zobrazeno 1 - 7
of 7
pro vyhledávání: '"S Avio"'
Publikováno v:
47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
In the frame of P80 Solid Rocket Motor Development it was developed the world largest monolithic composite case structure. Manufactured by the Italian company AVIO using filament winding technology, it achieved its formal q ualification end of 2009.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::872a6993f25896353293cc5f8d820ca2
https://doi.org/10.2514/6.2011-5958
https://doi.org/10.2514/6.2011-5958
Autor:
P. Perugini, A. Mataloni, F. Betti, Ernesto Vari, A. Leone, A. Di Cosmo, N. Tessitore, S Avio, Michel Bonnet
Publikováno v:
43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
In the framework of the VEGA European small launcher programme Avio has underway the parallel development and qualification of the composite cases of all the three solid propellant motor stages. The filament winding technology has enabled casings to
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4095f52f2277c04c93e0ad790eff3ce2
https://doi.org/10.2514/6.2007-5810
https://doi.org/10.2514/6.2007-5810
Publikováno v:
43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Aim of the present paper is to report the results of the three-dimensional numerical simulations of the unsteady, turbulent aerodynamic flow field around the VEGA launcher during stand-by on ground and lift-off phases. The unsteadiness of the flow fi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::346ad0b77361d8a3363996afd7003953
https://doi.org/10.2514/6.2007-5850
https://doi.org/10.2514/6.2007-5850
Publikováno v:
48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
This paper presents the studies performed within CNES, French Space Agency, in order to verify the integrity of the front composite skirt of the P80, first stage of VEGA European launcher. Being subjected to high compressive fluxes, the P80 skirt wit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ba8caa763288df3bc61927bfc15b2b93
https://doi.org/10.2514/6.2007-2120
https://doi.org/10.2514/6.2007-2120
Publikováno v:
43rd AIAA Aerospace Sciences Meeting and Exhibit.
Ignition and pres surization of the combu stion chamber are the most critical phases of a rocket’s launch. The aim of this work is to study these phenomena for a coaxial GCH4/GO2 injector representative of space applications. A simulation of this t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5e479e8f563c0879fa1da8bf18b9c75d
https://doi.org/10.2514/6.2005-742
https://doi.org/10.2514/6.2005-742
Publikováno v:
40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
An innovative FEM-based methodology for the investigation of damage tolerance behavior of a composite cases for Solid Rocket Motor is presented. The work has been developed in the frame of Vega Program. The aim of this program is to design and qualif
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e99cfb3bf1d1156364c0be95170d4e46
https://doi.org/10.2514/6.2004-4213
https://doi.org/10.2514/6.2004-4213
Publikováno v:
39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
This paper presents a technical and programmatic overview of the solid propellant motors designed for Vega, the new European Small Launch Vehicle developed under the responsibility of the European Space Agency. The prime contractor for the launch veh
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ae0009fd1204ece8874b22027a234683
https://doi.org/10.2514/6.2003-5284
https://doi.org/10.2514/6.2003-5284