Venus Express

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Venus Express
Venus Express in orbit
Mission typeVenus orbiter
OperatorEuropean Space Agency
COSPAR ID2005-045A Edit this at Wikidata
SATCAT no.28901
Websitewww.esa.int/venus
Mission durationPlanned: 2 years
Final: 9 years, 2 months, 9 days
Spacecraft properties
Manufacturer
EADS Astrium
Launch mass1,270 kg (2,800 lb)[1]
Dry mass700 kg (1,543 lb)[1]
Payload mass93 kg (205 lb)[1]
Dimensions1.5 × 1.8 × 1.4 m (4.9 × 5.9 × 4.6 ft)[1]
Power1,100 watts[1]
Start of mission
Launch date9 November 2005, 03:33:34 (2005-11-09UTC03:33:34) 
UTC[2]
RocketSoyuz-FG/Fregat
Launch siteBaikonur 31/6
ContractorStarsem
End of mission
DisposalDeorbited
Last contact18 January 2015, 15:01:55 (2015-01-18UTC15:01:56) 
UTC[3]
Decay dateJanuary / February 2015
Orbital parameters
Reference systemCytherocentric
Pericytherion altitude460 km (290 mi)[4]
Apocytherion altitude63,000 km (39,000 mi)[4]
Inclination90 degrees[5]
Period24 hours[5]
Venus orbiter
Orbital insertion11 April 2006
Venus Express mission insignia
ESA Solar System insignia for the Venus Express mission  

Venus Express (VEX) was the first

Venusian atmosphere. The observation over such long periods of time had never been done in previous missions to Venus, and was key to a better understanding of the atmospheric dynamics. ESA concluded the mission in December 2014.[6]

History

The mission was proposed in 2001 to reuse the design of the

Rosetta
spacecraft. The mission was proposed by a consortium led by D. Titov (Germany), E. Lellouch (France) and F. Taylor (United Kingdom).

The

Darmstadt, Germany
.

Seven further orbit control maneuvers, two with the main engine and five with the thrusters, were required for Venus Express to reach its final operational 24-hour orbit around Venus.[8]

Venus Express entered its target orbit at apoapsis on 7 May 2006 at 13:31 UTC, when the spacecraft was 151,000,000 kilometres (94,000,000 mi) from Earth. At this point the spacecraft was running on an

periapsis
was located almost above the North pole (80° North latitude), and it took 24 hours for the spacecraft to travel around the planet.

Venus Express studied the

Venusian atmosphere and clouds in detail, the plasma environment and the surface characteristics of Venus from orbit. It also made global maps of the Venusian surface temperatures. Its nominal mission was originally planned to last for 500 Earth days (approximately two Venusian sidereal days), but the mission was extended five times: first on 28 February 2007 until early May 2009; then on 4 February 2009 until 31 December 2009; and then on 7 October 2009 until 31 December 2012.[9] On 22 November 2010, the mission was extended to 2014.[10] On 20 June 2013, the mission was extended a final time until 2015.[11]

On 28 November 2014, mission control lost contact with Venus Express. Intermittent contact was reestablished on 3 December 2014, though there was no control over the spacecraft, likely due to exhaustion of propellant.

carrier signal was still being received from the vehicle, but no data was being transmitted. Mission manager Patrick Martin expected the spacecraft would fall below 150 kilometres (93 mi) in early January 2015, with destruction occurring in late January or early February.[13] The spacecraft's carrier signal was last detected by ESA on 18 January 2015.[3]

Instruments

ASPERA-4: An acronym for "Analyzer of Space Plasmas and Energetic Atoms," ASPERA-4 investigated the interaction between the solar wind and the Venusian atmosphere, determine the impact of plasma processes on the atmosphere, determine global distribution of plasma and neutral gas, study energetic neutral atoms, ions and electrons, and analyze other aspects of the near Venus environment. ASPERA-4 is a re-use of the ASPERA-3 design used on Mars Express, but adapted for the harsher near-Venus environment.

MAG: The magnetometer was designed to measure the strength of Venus's magnetic field and the direction of it as affected by the solar wind and Venus itself. It mapped the magnetosheath, magnetotail, ionosphere, and magnetic barrier in high resolution in three-dimensions, aid ASPERA-4 in the study of the interaction of the solar wind with the atmosphere of Venus, identify the boundaries between plasma regions, and carry planetary observations as well (such as the search for and characterization of Venus lightning). MAG was derived from the Rosetta lander's ROMAP instrument.

One measuring device was placed on the body of the craft. The identical second of the pair was placed the necessary distance away from the body by unfolding a 1 m long boom (carbon composite tube). Two redundant pyrotechnical cutters cut one loop of thin rope to free the power of metal springs. The driven knee lever rotated the boom perpendicularly outwards and latched it in place. Only the use of a pair of sensors together with the rotation of the probe allowed the spacecraft to resolve the small natural magnetic field beneath the disturbing fields of the probe itself. The measurements to identify the fields produced by the craft took place on the route from Earth to Venus.[14][15] The lack of magnetic cleanness was due to the reuse of the Mars Express spacecraft bus, which did not carry a magnetometer.[15] By combining the data from two-point simultaneous measurements and using software to identify and remove interference generated by Venus Express itself, it was possible to obtain results of a quality comparable to those produced by a magnetically clean craft.[15]

VMC: The Venus Monitoring Camera is a wide-angle, multi-channel

Technische Universität Braunschweig.[19] It is not to be confused with Visual Monitoring Camera mounted on Mars Express, of which it is an evolution.[17][20]

Venus Monitoring Camera channels[17]
VMC Channel Central Wavelength Spectral Range
VIS 513 nm 503 – 523 nm
NIR1 935 nm 900 – 970 nm
NIR2 1.01 µm 990 – 1030 nm
UV 365 nm 345 – 385 nm

PFS: The "Planetary Fourier Spectrometer" (PFS) should have operated in the

aerosols, and investigated surface to atmosphere exchange processes. The design was based on a spectrometer on Mars Express, but modified for optimal performance for the Venus Express mission. However PFS failed during its deployment and no useful data was transmitted.[21]

SPICAV: The "SPectroscopy for Investigation of Characteristics of the Atmosphere of Venus" (SPICAV) is an imaging spectrometer that was used for analyzing radiation in the infrared and ultraviolet wavelengths. It was derived from the SPICAM instrument flown on Mars Express. However, SPICAV had an additional channel known as SOIR (Solar Occultation at Infrared) that was used to observe the Sun through Venus's atmosphere in the infrared.

VIRTIS: The "Visible and Infrared Thermal Imaging Spectrometer" (VIRTIS) was an imaging spectrometer that observed in the near-ultraviolet, visible, and infrared parts of the electromagnetic spectrum. It analyzed all layers of the atmosphere, surface temperature and surface/atmosphere interaction phenomena.

VeRa: Venus Radio Science was a radio sounding experiment that transmitted radio waves from the spacecraft and passed them through the atmosphere or reflected them off the surface. These radio waves were received by a ground station on Earth for analysis of the ionosphere, atmosphere and surface of Venus. It was derived from the Radio Science Investigation instrument flown on Rosetta.

Science

Climate of Venus

Starting out in the early planetary system with similar sizes and chemical compositions, the histories of Venus and Earth have diverged in spectacular fashion. It is hoped that the Venus Express mission data that was obtained can contribute not only to an in-depth understanding of how the Venusian atmosphere is structured, but also to an understanding of the changes that led to the current greenhouse atmospheric conditions. Such an understanding may contribute to the study of climate change on Earth.[22][needs update]

Search for life on Earth

Venus Express was also used to observe signs of life on Earth from Venus orbit. In images acquired by the probe, Earth was less than one pixel in size, which mimics observations of Earth-sized planets in other planetary systems. These observations were then used to develop methods for habitability studies of exoplanets.[23]

Timeline of the mission

Animation of Venus Express's trajectory from 9 November 2005 to 31 December 2006
  Venus Express ·   Venus ·   Earth ·   Sun
Animation of Venus Express's trajectory around Venus from 1 April 2006 to 1 April 2008
  Venus Express ·   Venus
  • 3 August 2005: Venus Express completed its final phase of testing at
    Astrium Intespace facility in Toulouse, France
    .
  • 7 August 2005: Venus Express arrived at the airport of the Baikonur Cosmodrome.
  • 16 August 2005: First flight verification test completed.
  • 22 August 2005: Integrated System Test-3.
  • 30 August 2005: Last major system test successfully started.
  • 5 September 2005: Electrical testing successful.
  • 21 September 2005: FRR (Fuelling Readiness Review) Ongoing.
  • 12 October 2005: Mating to the Fregat upper stage completed.
  • 21 October 2005: Contamination detected inside the fairing – launch on hold.
  • 5 November 2005: Arrival at launch pad.
  • 9 November 2005: Launch from Baikonur Cosmodrome at 03:33:34 UTC.
  • 11 November 2005: First trajectory correction maneuver successfully performed.
  • 17 February 2006: The main engine is fired successfully in a dress rehearsal for the arrival maneuver.[24]
  • 24 February 2006: Second trajectory correction maneuver successfully performed.
  • 29 March 2006: Third trajectory correction maneuver successfully performed – on target for 11 April orbit insertion.
  • 7 April 2006: Command stack for orbit insertion maneuver is loaded on the spacecraft.
  • 11 April 2006: The Venus Orbit Insertion (VOI) is completed successfully, according to the following timeline:[25]
Event
Spacecraft event time
(UTC) 		Ground receive time (UTC)
Liquid Settling Phase start 07:07:56 07:14:41
VOI main engine start 07:10:29 07:17:14
periapsis passage 07:36:35
eclipse start 07:37:46
occultation start 07:38:30 07:45:15
occultation end 07:48:29 07:55:14
eclipse end 07:55:11
VOI burn end 08:00:42 08:07:28
Period of this initial orbit is nine days.[8]

See also

References

  1. ^ a b c d e "Venus Express Factsheet". European Space Agency. 1 June 2014. Retrieved 5 July 2017.
  2. ^ Siddiqi, Asif (2018). Beyond Earth: A Chronicle of Deep Space Exploration, 1958–2016 (PDF) (second ed.). NASA History Program Office.
  3. ^ a b c Scuka, Daniel (23 January 2015). "Venus Express: The Last Shout". European Space Agency. Retrieved 26 January 2015.
  4. ^ a b "Venturing into the upper atmosphere of Venus". European Space Agency. 11 November 2014. Retrieved 23 November 2014.
  5. ^ a b "Operational Orbit". European Space Agency. 14 December 2012. Retrieved 23 November 2014.
  6. ^ a b c Bauer, Markus; Svedhem, Håkan; Williams, Adam; Martin, Patrick (16 December 2014). "Venus Express goes gently into the night". European Space Agency. Retrieved 22 December 2014.
  7. ^ "Venus Express preliminary investigations bring encouraging news". ESA. 25 October 2005. Retrieved 9 May 2006.
  8. ^
    National Space Science Data Center
    . Retrieved 22 December 2014.
  9. ^ "Mission extensions approved for science missions". ESA. 16 October 2009.
  10. ^ "Europe maintains its presence on the final frontier". ESA. 22 November 2010.
  11. ^ "ESA science missions continue in overtime". ESA. 20 June 2013.
  12. ^ a b c "Venus Express anomaly". SpaceDaily. 8 December 2014. Retrieved 15 December 2014.
  13. ^ Drake, Nadia (17 December 2014). "Out of Fuel, Venus Express Is Falling Gently to Its Death in Planet's Skies". National Geographic. Archived from the original on 18 December 2014. Retrieved 22 December 2014.
  14. ^ "IWF : VEX-MAG". Iwf.oewa.ac.at. Archived from the original on 6 October 2014. Retrieved 15 December 2014.
  15. ^
    doi:10.5194/angeo-29-639-2011
    .
  16. ^ "The Venus Express mission camera". Max Planck Institute for Solar System Research. Archived from the original on 7 March 2008.
  17. ^ a b c Markiewicz, W. J.; Titov, D.; Fiethe, B.; Behnke, T.; Szemerey, I.; et al. "Venus Monitoring Camera for Venus Express" (PDF). Max Planck Institute for Solar System Research. Archived from the original (PDF) on 2 April 2015.
  18. ^ "Venus Monitoring Camera". Technical University at Brunswick.
  19. ^ "The light and dark of Venus". ESA. 21 February 2008.
  20. ^ Koeck, Ch.; Kemble, S.; Gautret, L.; Renard, P.; Faye, F. (October 2001). "Venus Express: Mission Definition Report" (PDF). European Space Agency. p. 17. ESA-SCI(2001)6.
  21. ^ Lakdawalla, Emily (23 July 2007). "Venus Express PFS fails to respond to a swift kick". The Planetary Society. Retrieved 2 February 2023.
  22. ^ "Atmospheric Dynamics of Venus and Earth" (PDF). Lpi.usra.edu. Retrieved 15 December 2014.
  23. ^ "Venus Express searching for life – on Earth". European Space Agency. Retrieved 15 December 2014.
  24. ^ "Successful Venus Express main engine test". European Space Agency. 17 February 2006. Retrieved 9 May 2006.
  25. ^ "Venus orbit insertion". European Space Agency. 24 May 2007. Retrieved 26 January 2015.
  26. ^ "The new temperature map of Venus' southern hemisphere". European Space Agency. 14 July 2009. Retrieved 27 November 2016.
  27. S2CID 129514118
    .
  28. ^ "Venus offers Earth climate clues". BBC News. 28 November 2007. Retrieved 29 November 2007.
  29. ^ "Venus Express Provides First Detection of Hydroxyl in Atmosphere of Venus". SpaceDaily. 20 May 2008. Retrieved 15 December 2014.
  30. ^ Carpenter, Jennifer (7 October 2011). "Venus springs ozone layer surprise". BBC News.
  31. hdl:2268/100136
    .
  32. ^ "A curious cold layer in the atmosphere of Venus". European Space Agency. 1 October 2012. Retrieved 15 December 2014.
  33. ^ Scuka, Daniel (16 May 2014). "Surfing an alien atmosphere". European Space Agency. Retrieved 23 November 2014.
  34. ^ "Venus Express rises again". European Space Agency. 11 July 2014. Retrieved 14 April 2015.

Further reading

External links

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