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Zefiro-9

Zefiro-9 is the solid third-stage motor shared by Vega and Vega-C. It draws on the Zefiro-16 demonstrator with improved composite structure, HTPB propellant, consumable igniters and electric actuators for the movable nozzle. ESA’s original Vega reference lists 117 s burn time and 313 kN maximum thrust. The final Vega-C qualification firing on 1 October 2020 burned approximately 10 tonnes of propellant for 120 s. These figures describe different reference and test conditions.

Identity

Domains
spaceflight
Identity Level
model
Kind
solid-rocket-motor
Name
Zefiro-9
Status
active

Details

Description
Zefiro-9 is the solid third-stage motor shared by Vega and Vega-C. It draws on the Zefiro-16 demonstrator with improved composite structure, HTPB propellant, consumable igniters and electric actuators for the movable nozzle. ESA’s original Vega reference lists 117 s burn time and 313 kN maximum thrust. The final Vega-C qualification firing on 1 October 2020 burned approximately 10 tonnes of propellant for 120 s. These figures describe different reference and test conditions.
First Flight Date
2012-02-13
Propellants
HTPB solid propellant
Rocket Specs
Burn Time
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Vacuum Thrust
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Links

Assets & Meta

Creation Time
July 29, 2026 at 09:08:53 UTC
Updated Time
October 29, 2026 at 15:57:06 UTC

Other

Diameter
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Sources