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Vega C

Vega C
Model of Vega C at Paris Air Show 2015
FunctionSmall-lift launch vehicle
ManufacturerAvio
Country of originEuropean multi-national[a]
Size
Height34.8 m (114 ft)
Diameter3.4 m (11 ft)
Mass210,000 kg (460,000 lb)
Stages4
Capacity
Payload to polar orbit
Altitude700 km (430 mi)
Orbital inclination90°
Mass2,300 kg (5,100 lb)
Associated rockets
FamilyVega
Comparable
Launch history
StatusActive
Launch sitesGuiana Space Centre, ELV
Total launches2
Success(es)1
Failure(s)1
First flight13 July 2022
First stage – P120C
Height11.7 m (38 ft)
Diameter3.4 m (11 ft)
Empty mass11,000 kg (24,000 lb)
Propellant mass143,600 kg (316,600 lb)
Maximum thrust4,500 kN (1,000,000 lbf)
Specific impulse278.5 s (2.731 km/s)
Burn time132.8 seconds
PropellantHTPB / AP
Second stage – Zefiro 40
Height7.6 m (25 ft)
Diameter2.3 m (7 ft 7 in)
Empty mass3,006 kg (6,627 lb)
Propellant mass36,200 kg (79,800 lb)
Maximum thrust1,304 kN (293,000 lbf)
Specific impulse293.5 s (2.878 km/s)
Burn time92.9 seconds
PropellantHTPB / AP
Third stage – Zefiro 9
Height4.12 m (13.5 ft)
Diameter1.9 m (6 ft 3 in)
Empty mass1,315 kg (2,899 lb)
Propellant mass10,500 kg (23,100 lb)
Maximum thrust314 kN (71,000 lbf)
Specific impulse296 s (2.90 km/s)
Burn time117 seconds
PropellantHTPB / AP
Fourth stage – AVUM+
Diameter1.5 m (4 ft 11 in)
Empty mass606 kg (1,336 lb)
Propellant mass740 kg (1,630 lb)
Powered by1 × RD-843
Maximum thrust2.42 kN (540 lbf)
Specific impulse314.6 s (3.085 km/s)
Burn time940 seconds

Vega C, or Vega Consolidation, is an expendable small-lift launch vehicle operated by Arianespace and developed and produced by Avio. It is an evolution of the original Vega launcher, designed to offer greater launch performance and flexibility. Development began after the December 2014 ESA Ministerial Council to address the need to accommodate larger institutional payloads and compete with more affordable launch providers.[1]

Like it's predecessor, Vega C is designed to launch small satellites for scientific and Earth observation missions to polar and low Earth orbits.[2] The reference Vega C mission is a polar orbit bringing a spacecraft of 2,300 kilograms (5,100 lb) to an altitude of 700 kilometres (430 mi), an increase of 800 kg (1,800 lb) over the original. The rocket, named after Vega, the brightest star in the constellation Lyra,[3] is a single-body launcher (no strap-on boosters) with three solid and one liquid stage. The lead manufacturer to the Vega program is from Italy, but the rocket has significant contributions from companies based in Belgium, France, Netherlands, Spain, Switzerland and Ukraine.

The Vega C incorporates several key improvements over the original Vega. The first-stage motor is replaced by the more potent P120C, a shared propulsion system with the Ariane 6 launcher. The second stage is the more powerful Zefiro 40, while the AVUM+ upper stage has more propellant than the original. The Zefiro 9 third stage remains unchanged.[4]

Vega rockets are launched from the ELV launch pad at the Guiana Space Centre. Vega C's maiden flight on 13 July 2022 successfully delivered LARES 2 and six other satellites to orbit.[5] However, the second launch on xx December 2022 experienced a failure of the Zefiro 40 second stage, resulting in the loss of two Pléiades Neo Earth-imaging satellites.[6] Consequently, the next launch was delayed until late 2024 to allow for the rocket motor nozzle to be redesigned.[7]

Specifications

Stages

Payload

Arianespace had indicated that the Vega launcher is able to carry 2,300 kg (5,100 lb) to a circular polar orbit at an altitude of 700 km (430 mi).[9]

Because of its ability to carry heavier payloads, RUAG Space of Switzerland had to redesign the fairing of the Vega C.

The fairing is 3.3 m (11 ft) in diameter and over 9 m (30 ft) tall, which offers nearly double the payload volume of the original Vega, which had a fairing of 2.6 m (8 ft 6 in) in diameter and over 7.8 m (26 ft) tall.[10]

Future

Building on Vega C, Vega E (or Vega Evolution) is a further evolution of the Vega C with the Zefiro 9 and AVUM+ third and fourth stage replaced with a cryogenic upper stage powered by liquid oxygen and liquid methane. This variant offers even more flexibility than Vega C, with the ability to deliver multiple satellites into different orbits on a single launch.[11]

As of March 2021 Avio is finalizing the development of the new M10 methane engine used in the new upper stage. The engine design is the result of a collaboration between Avio and Chemical Automatics Design Bureau (KBKhA) ended in 2014.[12]

Avio successfully conducted the first series of testing of the M10 engine between May and July 2022[13] with the maiden flight of the Vega-E planned for 2027.[14]

See also

Notes

  1. ^ The lead manufacturer is from Italy, but the rocket has significant contributions from companies based in Belgium, France, Netherlands, Spain, Switzerland and Ukraine.

References

  1. ^ "Media backgrounder for ESA Council at Ministerial Level". esa.int. ESA. 27 November 2014. Retrieved 2021-01-17.
  2. ^ Amos, Jonathan (13 February 2012). "Vega launcher makes first flight". BBC News. Retrieved 13 February 2012.
  3. ^ Tariq Malik (13 February 2012). "Europe Launches New Vega Rocket on Maiden Voyage". Space.com. Retrieved 29 May 2014. The Italian-built Vega rocket is named after the second-brightest star in the northern hemisphere
  4. ^ "VEGA C | Avio". avio.com. Avio. Retrieved 2021-01-17.
  5. ^ European Space Agency, ed. (2022-07-13). "Vega-C successfully completes inaugural flight". www.esa.int. Retrieved 2022-07-14.
  6. ^ "Europe's Vega C rocket fails on 2nd-ever mission, 2 satellites lost". Space.com. 21 December 2022.
  7. ^ Foust, Jeff (October 2, 2023). "ESA delays Vega C return to flight to late 2024". Spacenews.
  8. ^ "Vega C: What are the differences with Vega?". impulso.space. 2022-07-13. Retrieved 2024-07-03.
  9. ^ "Vega C — Overview". Arianespace.
  10. ^ "Vega-C". www.esa.int. Retrieved 2024-07-04.
  11. ^ "VEGA E | Avio". avio.com. Avio. Retrieved 2021-01-18.
  12. ^ P. Bellomi; M. Rudnykh; S. Carapellese; D. Liuzzi; G. Caggiano; L. Arione; A.A. Gurtovoy; S.D. Lobov; V. S. Rachuk (2019-02-08). "Development of LM10-MIRA liquid oxygen – liquid natural gas expander cycle demonstrator engine". Progress in Propulsion Physics – Volume 11. pp. 447–466. doi:10.1051/eucass/201911447. ISBN 978-5-94588-228-7. S2CID 139531422. Retrieved 2021-03-23.
  13. ^ "First Half 202 Results". Avio (Press release). 9 September 2022. Retrieved 16 September 2022.
  14. ^ "2023 half-year financial report" (PDF). Avio. Retrieved 10 September 2023.

External links

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