The industrial team is led by the French-Italian joint venture Europropulsion, under delegation from Avio SpA of Italy. Among the main industrial subcontractors involved in the P80 are SABCA of Belgium (thrust vector control system), Snecma Propulsion Solide of France (nozzle) and APP of the Netherlands (igniter).
ESA's Vega small satellite launcher is an all-solid-propellant, three-stage vehicle with a liquid-fuelled injection module, developed with the support of seven ESA Member States (Italy, France, Belgium, Switzerland, Spain, The Netherlands, and Sweden).
ELV SpA, a joint venture between Avio SpA and ASI, is the prime contractor for the Vega launcher development.
Vega is designed to lift single or multiple payloads to orbits of up to 1 500 km in altitude. Its baseline payload capability is to carry 1 500 kg to a circular, 700 km altitude, Sun-synchronous orbit. It can launch satellites ranging in mass from 300 kg to more than 2 tonnes.
This range of performance covers the needs of multiple applications in the fields of remote sensing, environmental monitoring, Earth science, space science, fundamental physics and research and technology for future space applications and systems.
Once qualified, Vega will be marketed and operated by Arianespace at the Guiana Space Centre, as a complement to Ariane 5 and Soyuz. It will serve the small to mid-sized satellite launch market.
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| Contact: Stefano Bianchi sfefano.bianchi@esa.int 39-069-418-0800 European Space Agency Source:Eurekalert |