• DocumentCode
    586477
  • Title

    Vega launch vehicle options to serve different satellites markets

  • Author

    Accettura, A.G. ; Genito, M.

  • Author_Institution
    Space Div., AVIO S.p.A., Rome, Italy
  • fYear
    2012
  • fDate
    2-5 Oct. 2012
  • Firstpage
    1
  • Lastpage
    4
  • Abstract
    The aim of this paper is to present different launch vehicle options in order to serve a wide range of satellites markets. These options are achieved through different vehicle architectures that can be synthesized by the following points: ; VEGA baseline configuration capable to serve mainly EO satellites on different mass ranges and arrangements; according to current performance capability we address payloads ranging from few kilograms up to 2 tons in LEO ; VEGA consolidation (VEGA-E1) with improved stages and associated technologies, this configuration allows a 2.4 tons in LEO payload ; VEGA evolution improved (VEGA-E2) could be capable to put 3.1 tons payload in LEO with 3 m fairing size ; VEGA evolution with an advanced propulsion module could serve ISS as well as high altitude missions; this version will be equipped with a debris mitigation system representing a breakthrough in launch vehicle operations. This vehicle constitute also a very low cost solar planets exploration system. For each vehicle a technology summary, a performance map and a mission profile will be shown. Launch vehicle design drivers for every option are the same that made VEGA baseline a mission success development programme, which are: LV launch service cost, customer & payload comfort, mission flexibility and the commonality with the Ariane family. Regarding the last point, the complementary with respect to existing family fleet (Soyuz and Ariane) has been considered in order to make the best possible synergy among launch systems, also completing the European launch capability. It is worth to note that VEGA launchers will be capable to serve both consolidated and emerging satellite markets. In particular, a service market-matrix showing benefits for citizens worldwide will be shown and explicated, also taking into consideration the contribution to the global space value chain (i.e. impacts on everyday life, human activities monitoring, natural disaster mitigation and so on). Finally- a roadmap to address future developments will be proposed and an overall operational scenario will be presented.
  • Keywords
    artificial satellites; satellite communication; Ariane family; European launch capability; ISS; LEO payload; LEO satellites; LV launch service cost; VEGA baseline configuration; VEGA consolidation; VEGA-E1; VEGA-E2; Vega launch vehicle; debris mitigation system; high altitude missions; launch vehicle design; mission profile; payload comfort; satellites markets; service market-matrix; vehicle architectures; very low cost solar planets exploration system; Europe; Low earth orbit satellites; Orbits; Payloads; Propulsion; Vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Satellite Telecommunications (ESTEL), 2012 IEEE First AESS European Conference on
  • Conference_Location
    Rome
  • Print_ISBN
    978-1-4673-4687-0
  • Electronic_ISBN
    978-1-4673-4686-3
  • Type

    conf

  • DOI
    10.1109/ESTEL.2012.6400203
  • Filename
    6400203