Vega C R2

Vega family

VEGA C

The new configuration of the Vega rocket is called the Vega C (Consolidation) and offers an improved performance. The new launcher vehicle is capable to lift up to 2,300 kg in Low Earth Orbit (+60%). 

Vega C takes full advantage of the capabilities of the new SSMS (Small Spacecraft Mission Service) payload adapter to transport dozens of microsatellites in Low Earth Orbit. In addition, the launcher has been ichosen for the first launch of the European Space Rider experimental spacecraft.

The maiden flight of Vega C took place on July 13th 2022

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VEGA C

Main CHARACTERISTICS

The new Vega C launcher is more flexible and versatile than its predecessor, increasing the market for this vehicle from 50% to 90% of LEO satellites, a substantial part of which can be managed by exploiting its multiple launch capability. From this standpoint, the VESPA+R Payload Adapter is used in missions involving multiple launches (two satellites) or to house Cubesats and microsats in its internal platform.

capabilities and architecture

A further major innovation is the Small Spacecraft Mission Service (SSMS), an adapter, also under development, which enables the Vega C to increase the quantity of miniaturized satellites carried on each single launch.

The architecture of Vega C is based on the existing Vega launcher. Specifically, like its predecessor, Vega C consists of 3 stages based on solid propulsion motors and one stage based on a liquid propulsion engine.

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Vega C Wire

Vega C

P120 C MOTOR

Main Data

MOTOR LENGTHmeters13,5
DIAMETERmeters3,4
PROPELLANT MASStons141,4
MOTOR DRY MASSkg11.200
Motor case masskg8.200
MAXIMUM THRUSTkn4780
Specific impulseseconds280,0
Combustion timeseconds134
Vega P120

vega c

ZEFIRO 40

Main Data

MOTOR LENGTHmeters7,6
DIAMETERmeters2,3
PROPELLANT MASStons36,1
MOTOR DRY MASSkg3.230
Motor case masskg2.130
Average thrust kn1.035
Specific impulseseconds292,2
Combustion timeseconds99,8
Vega Z40

vega c

Zefiro 9

Main Data

MOTOR LENGTHmeters3,9
DIAMETERmeters1,9
PROPELLANT MASStons10,5
MOTOR DRY MASSkg929
Motor case masskg630
Average thrust kn255
Specific impulseseconds294,8
Combustion timeseconds119,2
Vega Z9

vega c

AVUM+

Main Data

DIAMETERmeters2
PROPELLANT MASSkg737
Mass of inertskg695
MOTOR MASSkg16
Specific impulseseconds316,3
Combustion timeseconds892
Average thrust of the main motorkn2,47
Vega Avum

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