VEGA: 1° stage - P80 Motor -
page-template,page-template-full_width,page-template-full_width-php,page,page-id-2412,page-child,parent-pageid-2647,eltd-cpt-1.0,,avio theme-child-ver-1.0,moose-ver-1.7, vertical_menu_with_scroll,smooth_scroll,blog_installed,wpb-js-composer js-comp-ver-5.0.1,vc_responsive

VEGA: 1° stage – P80 Motor


It’s the solid-propellant first stage of the Vega Launcher. At present, it’s the largest single-unit, solid-propellant engine ever built with Filament Winding technology.
Almost 11 metres tall and with a diameter of 3 metres, it weighs 95 tonnes and burns around 88 tonnes of solid propellant in slightly less than 2 minutes. The P80 generates 300 tonnes of thrust – the same amount produced by four jumbo jets on take-off.
The first static bench test was successfully completed in late 2006 at the Kourou Space Centre in French Guyana. The results were confirmed in late 2007, when the P80 fully passed its qualifying test, again at Kourou.

Main characteristics

  • Motor length: 10,6 m
  • Diameter: 3 m
  • Propellant mass: 88 t
  • Motor dry mass: 7.330 kg
  • Motor case mass: 3.260 kg
  • Average thrust: 3015 kN
  • Specific impulse: 280 s
  • Combustion time: 110 s

By using this website, you agree to accept our cookie policy. find out more

Questo sito utilizza i cookie per fornire la migliore esperienza di navigazione possibile. Continuando a utilizzare questo sito senza modificare le impostazioni dei cookie o cliccando su "Accetta" permetti il loro utilizzo.