Vega (rocket)

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Vega
Vega rocket
Vega rocket
Function Small orbital launch vehicle
Manufacturer ESA/ASI/Avio
Country of origin Europe
Size
Height 30 m (98 ft)
Diameter 3 m (9.8 ft)
Mass 137,000 kg (300,000 lb)
Stages 4
Capacity
Payload to LEO 1,500 kg (3,300 lb)
Launch history
Status Active
Launch sites ZLV (ELA-1), Centre Spatial Guyanais
Maiden flight 13 February 2012 (2012-02-13) at 10:00 UTC[1]
First stage
Engines 1 P80
Thrust 3040 kN
Burn time 107 seconds
Fuel Solid
Second stage
Engines 1 Zefiro 23
Thrust 1200 kN
Burn time 71.6 seconds
Fuel Solid
Third stage
Engines 1 Zefiro 9
Thrust 213 kN
Burn time 117 seconds
Fuel Solid
Fourth stage
Engines 1 RD-869
Thrust 2.45 kN
Burn time 315.2 seconds
Fuel UDMH/N2O4

Vega (Vettore Europeo di Generazione Avanzata,[2] Advanced Generation European Carrier Rocket) is an expendable launch system in use by Arianespace jointly developed by the Italian Space Agency and the European Space Agency. Development began in 1998 and the first launch took place from the Guiana Space Centre on 13 February 2012.[3]

It is designed to launch small payloads — 300 to 2,500 kg satellites for scientific and Earth observation missions to polar and low Earth orbits.[4] The reference Vega mission is a polar orbit bringing a spacecraft of 1,500 kilograms to an altitude of 700 kilometers.

Vega is a single-body launcher (no strap-on boosters) with three solid rocket stages, the P80 first stage, the Zefiro 23 second stage, the Zefiro 9 third stage, and a liquid rocket upper module called AVUM. The technology developed for the P80 program will also be used for future Ariane developments. Italy is the leading contributor to the Vega program (60%), followed by France (25%).[5] Other participants include Spain, Belgium, The Netherlands, Switzerland and Sweden.[6]

Contents

[edit] Payload capacity

Arianespace indicates a Vega launcher is able to carry 1,500 kilograms (3,300 lb) to a circular polar orbit at an altitude of 700 kilometres (430 mi).[7]

Arianespace is marketing Vega as a launch system tailored for missions to low Earth and sun-synchronous orbits.[8] In its qualification flight VEGA put its main payload of 386.8 kg, the LARES satellite, into a circular orbit at the altitude of 1450 km with an inclination of 69.5 degrees.[9]

[edit] Specifications

To compare with other current or retired rockets:[citation needed]

Specification Vega Ariane 1
(retired)		 Rokot[10] Dnepr-1 Taurus
Lift off mass 136 t 210 t 107 t 211 t 73 t
Height 30 m 47.40 m 29.15 m 34.3 m 27.9 m
Diameter 3 m 3.80 m 2.50 m 3 m 2.35 m
Heliosynchron orbit payload 0.3 t –
2.5 t
LEO payload 1.5 t – 2 t 1.95 t
(LEO, 200 km, 63°)		 4.5 t
(LEO, 200 km, 66°)		 1.35 t
Polar orbit payload 1.5 t 1,200 kg
600 km, 98°
Success rate 1 from 1 9 from 11 16 from 18 16 from 17 6 from 9

[edit] Four stages

[citation needed] First Stage Second Stage Third Stage Fourth Stage
Propulsion P80 Zefiro 23 Zefiro 9 AVUM
Height 10.5 m 7.5 m 3.85 m 1.74 m
Diameter 3 m 1.9 m 1.9 m 1.9 m
Propellant mass 88 t 23.9 t 10.1 t 0.55 t
Thrust (max) 3,040 kN (683,420 lbf) 1,200 kN (269,770 lbf) 213 kN (47,880 lbf) 2.45 kN (550 lbf)
Nozzle expansion ratio 16 25 56 –
Burn time 107 s 71.6 s 117 s 317 s
Specific impulse 279.5 s 289 s 294 s 315.2 s

[edit] Three solid motor stages

The first three stages are solid propellant engines produced by Avio, that is Prime Contractor for the Vega launcher through its company ELV.[11]

Each of the three engine types intended for the three stages of the Vega had to be commissioned with two test-launches — one for design evaluation, one in final flight configuration.[citation needed]

[edit] Zefiro 9

The first engine completed was Zefiro 9, the third stage engine. The first test firing was carried out on 20 December 2005, at the Salto di Quirra Inter-force Test Range, on the Mediterranean coast in southeast Sardinia. The test was a complete success.[12]

After a critical design review based on the completed first test firings,[13] the second test-firing of the Zefiro 9 took place at Salto di Quirra on 28 March 2007. After 35 seconds, there was a sudden drop in the motor's internal pressure, leading to an increased combustion time.[14] No public information is available for this sudden drop of internal pressure, and what if any flaws were present in the motor's design.

On 23 October 2008 an enhanced version of the Zefiro 9 with a modified nozzle design, the Zefiro 9-A, was successfully tested.[15]

On 28 April 2009, the final qualification test firing of Zefiro 9-A took place at the Salto di Quirra Interforce Test Range in Sardinia, Italy.[16]

[edit] Zefiro 23

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. A Zefiro 23 forms the second stage of Vega. Its carbon-epoxy case is filament-wound and its carbon phenolic nozzle includes a carbon-carbon throat insert. The propellant loading is 23 tons.[17]

The Zefiro 23 second stage engine was first fired on 26 June 2006 at Salto di Quirra. This test was successful.[18]

The second test firing of the Zefiro 23 second stage engine took place on 27 March 2008 also at Salto di Quirra. This successful test qualified the rocket engine.[19]

[edit] P80

The P80 first stage also uses a filament-wound case. Its nozzle uses a flexible joint that is electrically actuated.[17]

The first test firing of the P80 engine took place on 30 November 2006 in Kourou, and the test was concluded successfully.[20]

The second test firing of the P80 first stage engine took place on 4 December 2007 in Kourou. Delivering a mean thrust of 190 tonnes over 111 seconds, the engine's behaviour was in line with predictions.[21]

[edit] AVUM

The AVUM (Attitude Vernier Upper Module) upper module consists of a propulsion module and an avionics module. The module uses a RD-869 rocket engine liquid-fuel rocket burning pressure-fed UDMH and nitrogen tetroxide as propellants, built by Yuzhnoye Design Bureau.[6][22] The AVUM avionics module contains the main components of the avionics sub-system of the vehicle.[23]

[edit] Flights

[edit] Lead-up to first launch

Enrico Saggese, at that time head of the Italian Space Agency, suggested in October 2008 that the first flight of VEGA might be delayed, stating "We have to decide if we want to wait until we have another programme", and referring to plans to have German participation to develop new third and fourth stages.[24]

In 2009 the first launch of the system was anticipated to take place in November 2010;[25][26] later press suggested that the launch would slip to early 2012, until ESA publicized the launch for "end of January 2012".[27]

[edit] Vega launches

The maiden flight occurred on 13 February 2012.[28]

No. Date/Time
(UTC)		 Type Serial-no. Startplace Payload Type of payload Orbit Outcome Remarks
1 13 February 2012
10:00		 Vega VV01 ELV
(previous ELA-1)		 LARES / ALMASat 1 / e-st@r / Goliat / MaSat-1 / PW-Sat 1 / ROBUSTA / UniCubeSat-GG / XaTcobeo Geodetic and nanosatellites LEO orbit Success First Vega launch

[edit] Planned future launches

Having successfully completed the maiden qualification flight, ESA has plans for a second flight, followed by four more flights in its "VERTA programme."[29]

The Italian Aerospace Research Centre plans to launch its "FTB-X" test vehicle on a Vega launcher in 2012.[30]

Vega could be designated to put Proba-V in orbit.[31]

In a meeting held on 14 December 2011 in Evry, France, representatives from Arianespace and the European Space Agency (ESA) signed a contract that binds the company to launch the Sentinel-2B and Sentinel-3B satellites aboard a Vega rocket.[32]

Vega is presently the baseline vehicle for LISA Pathfinder. The launch is expected in June 2013.[33]

[edit] Costs

Developments costs for the Vega rocket were €710 million, with ESA spending an additional €400 million to sponsor five development flights between 2012 and 2014.[34] Commercial launches will be sold for €32 million, a price set to compete with converted Russian ballistic missiles.[35]

[edit] Future developments

There was a concept study for a new medium-size launcher based on Vega and Ariane 5 elements. This launcher would use an Ariane 5 P230 first stage, a Vega P80 second stage and an Ariane 5 third stage using either storable or cryogenic fuel.[17] The addition of Soyuz to the Arianespace launch vehicle lineup removed momentum from this initiative.[citation needed]

The future upgraded Vega (LYRA program) has exceeded the feasibility study and is planned to have new third and fourth low cost LOX/HC stages and a new guidance system. The purpose of the program is to upgrade the performance by about 30% without significant price increase.[36]

On 14 February 2012, one day after the successful first launch of Vega, the German space agency moved to be included in the program. Johann-Dietrich Woerner, head of the German Aerospace Agency DLR, said Germany wanted to join the project. Germany would provide a replacement for the RD-869 engine on the AVUM fourth stage, currently made in Ukraine. The Vega Launcher Manager stated that it will not fly in the near future because it takes some time to develop, but he confirmed it will be on agenda in the next meeting of ministers in late 2012. That way, all components of the rocket would be built inside the EU.[37]

[edit] See also

[edit] References

  1. ^ "Vega liftoff". ESA. http://www.esa.int/esaCP/SEMBTKYXHYG_index_0.html. 
  2. ^ ESA: Antonio Fabrizi: from "nuts and bolts" to Europe’s launchers of today and tomorrow [1]
  3. ^ "ESA – Vega". Esa.int. 3 February 2012. http://www.esa.int/SPECIALS/Vega/index.html. Retrieved 14 February 2012. 
  4. ^ Amos, Jonathan (13 February 2012). "Vega launcher makes first flight". BBC News. http://www.bbc.co.uk/news/science-environment-16956324. Retrieved 13 February 2012. 
  5. ^ "Vega Launcher Targets Government Market". Aviation Week. 6 February 2012. http://www.aviationweek.com/aw/generic/story_channel.jsp?channel=space&id=news/awst/2012/02/06/AW_02_06_2012_p50-420459.xml&headline=Vega%20Launcher%20Targets%20Government%20Market. Retrieved 14 February 2012. 
  6. ^ a b CLARK, S. (14 February 2012). "Vega launcher program courts German participation". Spaceflight Now. pp. 1. http://www.spaceflightnow.com/news/n1202/14germanyvega/. Retrieved 14 February 2012. 
  7. ^ "Vega — Overview". Arianespace. http://www.arianespace.com/launch-services-vega/vega_overview.asp. 
  8. ^ "Vega — Performance". Arianespace. http://www.arianespace.com/launch-services-vega/performance.asp. 
  9. ^ I. Ciufolini et al. The Design of LARES: A Satellite for Testing General Relativity, IAC-07-B4.2.07, proceedings of the 58th International Astronautical Congress, India, Hyderabad, 2007
  10. ^ Rockot
  11. ^ "Space Propulsion". Aviogroup.com. http://www.aviogroup.com/en/catalog/space/propulsione_spaziale. Retrieved 16 February 2012. 
  12. ^ ESA: Successful first test for Vega's Zefiro 9 engine
  13. ^ ESA: Vega Critical Design Review begins
  14. ^ ESA: Anomalous behaviour affects firing test of Vega’s Zefiro 9 motor
  15. ^ "Successful first test for Vega’s Zefiro 9-A solid-fuel rocket motor". ESA. 24 October 2008. http://www.esa.int/esaCP/SEM0KERTKMF_index_1.html. 
  16. ^ "Successful second test for Vega’s Zefiro 9-A solid-fuel rocket motor". ESA. 30 April 2009. http://www.esa.int/esaCP/SEM688BNJTF_index_0.html. 
  17. ^ a b c M. Caporicci (November 2000). "The Future of European Launchers: The ESA Perspective". ESA. http://www.esa.int/esapub/bulletin/bullet104/caporicci104.pdf. 
  18. ^ ESA: Vega's second stage motor roars to life
  19. ^ Successful qualification firing test for Zefiro 23
  20. ^ ESA: Successful firing of Vega’s first-stage motor in Kourou
  21. ^ ESA: Vega main engine test in Kourou
  22. ^ "The Ukrainian engine operated successfully on the new European rocket". Youzhnoye KB. 14 February 2012. http://www.yuzhnoye.com/index.php?idD=91&id=124&path=News/News_e&lang=en. Retrieved 14 February 2012. 
  23. ^ "Vega Launcher". ESA. 6 February 2012. http://www.esa.int/SPECIALS/Vega/SEMNLCWWVUG_0.html. Retrieved 16 February 2012. 
  24. ^ "Italian Space Agency Plans its Relaunch". Flight International. 31 October 2008. http://www.flightglobal.com/articles/2008/10/31/318226/italian-space-agency-plans-its-relaunch.html. 
  25. ^ "Avio: Vega's motors qualify but maiden launch slips to 2010". Flight International. 29 April 2009. http://www.flightglobal.com/blogs/hyperbola/2009/04/new-european-vega-rockets-soli.html. 
  26. ^ "Delays seen for Soyuz, VEGA launches at Europe's Space Base". 15 June 2009. http://www.google.com/hostednews/afp/article/ALeqM5jlKAnEb0VTqJUW7tVWXxmIrryWIQ. 
  27. ^ "Vega moves closer to its first liftoff". ESA. 15 December 2011. http://www.esa.int/SPECIALS/Launchers_Home/SEMS0T7XZVG_0.html. 
  28. ^ "ESA’s new Vega launcher scores success on maiden flight.". http://www.esa.int/SPECIALS/Vega/. 
  29. ^ "Announcement of opportunity for second flight of Vega small launcher in mid-2010". ESA. 25 July 2008. http://www.esa.int/SPECIALS/Launchers_Home/SEM3MKXIPIF_0.html. 
  30. ^ Tariq Malik (12 March 2007). "Italian Firm Hails Test of Unmanned Spacecraft Prototype". http://www.space.com/businesstechnology/070312_usv_droptest.html. 
  31. ^ ESA (3 November 2010). "About Proba-V". http://www.esa.int/esaMI/Proba/SEM9FS4PVFG_0.html. 
  32. ^ Tudor Vieru (19 December 2011). "Vega Rocket to Launch Two ESA Sentinel Satellites". http://news.softpedia.com/news/Vega-Rocket-to-Launch-Two-ESA-Sentinel-Satellites-241417.shtml. 
  33. ^ ESA (25 January 2011). "LISA Pathfinder". http://www.esa.int/esaMI/Operations/SEMR4E7DWZE_0.html. 
  34. ^ de Selding, Peter B. (2012-02-13). "Europe’s Italian-led Vega Rocket Succeeds in Debut". SPACE NEWS. http://www.spacenews.com/launch/120213-vega-succeeds-debut.html. 
  35. ^ Messier, Doug (2012-02-16). "Officials Eye New Upper Stage for Vega Rocket". Parabolic Arc. http://www.parabolicarc.com/2012/02/16/officials-eye-new-upper-stage-for-vega-rocket/. 
  36. ^ ""LIRA". Agenzia Spaziale Italiana. http://www.asi.it/en/activity/transportation/lyra. Retrieved 17 February 2012. 
  37. ^ CLARK, S. (14 February 2012). ""Vega launcher program courts German participation"". Spaceflight Now. pp. 1. http://www.spaceflightnow.com/news/n1202/14germanyvega/. Retrieved 14 February 2012. 

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