Vega Satellite Launch Vehicle

The Vega (Vettore Europeo di Generazione Avanzata) is a new-generation launch vehicle being developed jointly by the Italian Space Agency (ASI) and the European Space Agency (ESA) for Arianespace.

Vega is named after the second brightest star in the northern hemisphere.

The Vega is a small launcher which can place small to medium-sized satellites into the polar and low-earth orbits. The launch vehicle complements the heavy Ariane 5 and medium Soyuz rockets launched from French Guiana.

Vega development programme history

“The Vega is a small launcher which can place small to medium-sized satellites into the polar and low-earth orbits.”

The development of the Vega launcher commenced under the Vega programme in 1998. The programme is being funded by Italy (65%), France (12.43%), Spain (5%), Belgium (5.63%), the Netherlands (3.5%), Switzerland (1.34%) and Sweden (0.8%).

Vega’s main engine P80 rocket motor was successfully tested in December 2007. The test campaign of the Vega launch vehicle commenced in November 2010.

The test phase validated the operational readiness of the launch vehicle and ground station components. The assembly of the new Vega launcher was completed in February 2011.

The first launch is scheduled for February 2012 from Europe’s Spaceport in French Guiana. ESA plans to launch its IXV (intermediate eXperimental vehicle) aboard Vega in 2014.

The marketing activities will commence after the first launch. Arianespace plans to increase the launch frequency from two to four each year.


ASI and Avio have established a new 30-70 partnership called Elv for the programme. ESA and Elv signed the Vega development contract in February 2003.

Elv, as the prime contractor, is responsible for the management of the Vega programme. The company also coordinates the activities of the subcontractors involved. Arianespace provides support services for the qualification and combined test campaign of the rocket.

In December 2011, ESA and the Arianespace signed a contract to study the launch of Vega under the Verta (Vega Research and Technology Accompaniment) programme. The programme will test and qualify new vital technologies for future re-entry vehicles.

Vega design

The Vega launch vehicle is designed to support various missions and payload configurations in order to meet different market requirements. It offers payload configurations from a single satellite to one primary satellite plus six micro-satellites.

“ASI and Avio have established a new 30-70 partnership called Elv for the programme. ESA and Elv signed the Vega development contract in February 2003.”

Vega can place multiple payloads into orbit which is uncommon with most small launchers. It can carry payloads of 300kg to 2,500kg based on the type and altitude of the orbit required by the customers.

The vehicle has a length of 29.9m, a diameter of 3.025m and a typical lift-off mass of 137t.

The in-orbit launch capacity of the vehicle is 1,500kg into the polar orbit at an altitude of 700km. The single body launcher is incorporated with three solid propulsion stages and an AVUM (attitude vernier upper module).

The solid propellant motors, supplied by Avio, are covered by composite casing. The motors feature carbon epoxy filament wound casing and nozzle.

The first stage is powered by the P80 solid rocket motor. The second and third stages are powered by Zefiro 23 and Zefiro 9 motors respectively. The fourth stage AVUM consists of a UDMH / NTO bipropellant main engine with re-ignition capability and cold gas attitude control system.

Vega launch facilities

The Vega will be launched from ZLV launch complex at Kourou, French Guiana. Based on the ELA-1 (Ensemble de Lancement Ariane No. 1) launch complex, the site was originally used for the Ariane 1 and Ariane 3 vehicles.

The existing facilities, such as the launch pad, mobile gantry and infrastructure, were upgraded for the launch of the Vega.

The original flame ducts of the launch pad were retained. They will transfer exhaust gases during ignition and lift-off of the Vega.

The power and environmental control connections to the launcher and its payloads are provided by a new fixed umbilical mast. Four tall towers erected around the launch table will provide protection against lightning strikes.

The renovated mobile gantry provides provides ideal working conditions to the personnel during the launch vehicle assembly and payload integration.

The operational control centre for the Vega will be within the Spaceport’s Control Centre no. 3 (CDL 3) facility, which is used for Ariane 5 missions. The centre incorporates independent operational control and monitoring systems. The Vega facility will share resources with the ongoing Ariane 5 mission as it is co-located in the CDL-3 building. Continue reading

Vega rocket ready for first flight


Vega VV01 liftoff
Flight VV01

Vega rocket ready for first flight

19 January 2012
Final checkout of Europe’s new Vega launcher was completed last Friday, marking another milestone towards its maiden flight from Europe’s Spaceport in Kourou, French Guiana.

The first Vega launch campaign began in November with the installation of the P80 first stage on the launch pad. The two solid-propellant second and third stages were added to the vehicle, followed by the AVUM – Attitude & Vernier Upper Module – liquid-propellant fourth stage.  

AVUM pressurisation
AVUM pressurisation

All four stages have undergone final acceptance, including the testing of the avionics, guidance, telemetry, propulsion, separation pyrotechnics and safety systems.These steps culminated on 13 January with Vega’s ‘synthesis control checks’, where all systems were put into launch mode for the vehicle’s final acceptance. This included pressurising the AVUM propulsion systems that actuate the thruster valves.

The rocket’s elements were switched on from the control bench to simulate the launch countdown. The onboard software then took over and simulated the different stages of a flight. The interfaces between the vehicle and the control bench were also tested.

The test review confirmed that everything ran as expected and that the launcher is ready for flight.

AVUM in mobile gantry

What’s next?

The ‘upper composite’ – the fairing and payload – will be integrated, followed by final checkout of the fully assembled launcher and the countdown rehearsal.

The first launch, VV01, is targeted for 9 February. It will carry nine satellites into orbit: the Italian space agency’s LARES and ALMASat-1, together with seven CubeSats from European universities.

This mission aims to qualify the Vega launch system, including the vehicle, its launch infrastructure and operations, from the launch campaign to payload separation and disposal of the upper module.

Artist's impression of Vega
Vehicle VV01

A flexible system

Vega is designed to cope with a wide range of missions and payload configurations in order to respond to different market opportunities and provide great flexibility.

In particular, it offers configurations able to handle payloads ranging from a single satellite up to one main satellite plus six microsatellites.

Vega is compatible with payload masses ranging from 300 kg to 2500 kg, depending on the type and altitude of the orbit required by the customers. The benchmark is for 1500 kg into a 700 km-altitude polar orbit.

More information on Vega and updates are now available on the new launch website here.