Italy is the leading contributor to the Vega program (65%), followed by France (13%). The test was a complete success.[77]. [14] This proposed launcher, dubbed Vega, was promoted as functioning to expand the range of European launch capabilities; Vega would be capable of launching a 1000 kg payload into a 700 km polar orbit. Thrusters will typically burn one, two or more times to reach the required orbits. [74], The development of the Zefiro motor was initiated by Avio, partially funded by the company and partially funded by a contract from the Italian Space Agency.

The AVUM avionics module contains the main components of the avionics sub-system of the vehicle. Vega (Italian: Vettore Europeo di Generazione Avanzata, meaning "Advanced generation European carrier rocket"), is an expendable launch system in use by Arianespace jointly developed by the Italian Space Agency (ASI) and the European Space Agency (ESA). Vega (Italian: Vettore Europeo di Generazione Avanzata,[9] meaning "Advanced generation European carrier rocket"),[9] is an expendable launch system in use by Arianespace jointly developed by the Italian Space Agency (ASI) and the European Space Agency (ESA). After a critical design review based on the completed first test firings,[78] the second test-firing of the Zefiro 9 took place at Salto di Quirra on 28 March 2007.

This test was successful. The German Aerospace Center (DLR) was reportedly enthusiastic on the prospects of developing a European alternative to the Vega's final, fourth stage; however, it was widely believed that there should be no change to Vega hardware for roughly 10 years in order to consolidate operations and avoid unnecessary costs early on.

 #ASE2B032RNC th { background-color: #ffffff; color: #ff0000; } #ASE2B032RNC { border-collapse: collapse; } #ASE2B032RNC td, #ASE2B032RNC th { border: 1px solid #999999; }. It is designed to launch small payloads — 300 to 2500 kg satellites for scientific and Earth observation missions to polar and low Earth orbits. The solid rocket motors built for Vega-C under contract to Avio have all completed the … [47][52] On 13 February 2012, the first launch of the Vega rocket occurred for Kourou; it was reported as being an "apparently perfect flight".

[66] It has a diameter of 2.6 metres, a height of 7.8 metres and a mass of 400 kg. * Launch in circular orbit, 90°inclination, 700 km, function win1(){ msgWindow=window.open('https://ravel.esrin.esa.it/multimedia/vega/index_vega.html','newWin1', 'resizable=no,width=440,height=540,top=0,left=0,noresize,scrollbars=no'); }. Using a new range of payload carriers, Vega-C will be able to accommodate cargo of different shapes and sizes ranging from multiple small satellites as small as one kilogram up to a single large payload. [31][32] In September 2005, the successful completion of key tests on the Vega's solid rocket motor igniters, a key milestone, was reported. Costs are being kept to a minimum by using advanced low-cost technologies and by introducing an optimised synergy with existing production facilities used for Ariane launchers.

Development of the Vega launcher started in 1998. ESA is working with industry towards the first flight of Europe’s Vega-C launch vehicle for more launches, with increased performance, reaching multiple orbits at a similar cost to Vega. [70] The 3 m diameter case is composed of graphite epoxy filament wound case and low density rubber is used for the internal insulation.

Vega has been designed as a single body launcher with three solid propulsion stages and an additional liquid propulsion upper module used for attitude and orbit control, and satellite release.

[23][24], Around 2000, an alternative use for the Vega was explored as a medium-class booster rocket to be used in conjunction with an improved, up-rated model of the Ariane 5 heavy launcher. [73], The future version of the stage, P120C, also with its name derived from the design phase propellant weight of 120 tons, will increase the propellant mass to 141-143 tons. The Small Spacecraft Mission Service (SSMS) dispenser will allow dedicated rideshares to space.

The AVUM consists of two modules: AVUM Propulsion Module (APM) and AVUM Avionics Module (AAM). Routine dedicated rideshares to space for small satellites. Enabling & Support First Vega launch campaign aims for January liftoff. Read. [22] In November 1999, European Space Agency (ESA) formally dropped Vega as an endorsed programme, a decision which was largely attributed to France's withdrawal; Italy declared that it would proceed regardless, and threatened to re-direct its allocated contributions for the further development of the Ariane 5 to meet the shortfall. This will meet the needs of European institutions and industry.

[29] In May 2004, it was reported that a contract was signed between commercial operator Arianespace and prime contractor ELV to perform vehicle integration at Kourou, French Guiana. Return missionsThe Space Rider system under development will be launched on Vega-C and use the AVUM+ upper stage capabilities to provide in-orbit operations for payload return capability. Single large passengerThe Vampire will be used for single large payloads with possible combination with the smaller payloads on the SSMS multiple payload dispenser.

Vega-C is a single body rocket about 35 m high with a mass at liftoff of 210 tonnes. PARIS (ESA PR) — Europe’s new-generation Vega-C small launch vehicle developed by ESA will increase performance and extend current launch capabilities at Europe’s Spaceport..

The first stage P120C motor is one of the largest monolithic carbon-fibre solid-propellant rocket motors ever built in one piece.

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