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European Venus Explorer

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The European Venus Explorer (EVE), known until 2007 as the Venus Entry Probe (VEP), is a proposed European Space Agency space probe to Venus. In the timeline of the 2005 TRS (technology reference study), the spacecraft was proposed to be launched on a Soyuz-2/Fregat launch vehicle around 2013. However, requests to fund and develop the spacecraft in 2007 and 2010 were rejected.

EVE was a Medium-Class mission proposal in the Cosmic Vision programme. The mission concept consisted of an orbiter and balloon which would circumnavigate the planet over the course of one week, and a lander probe which would operate for approximately one hour on the surface.

Overview

The mission concept calls for two satellites: the Venus Polar Orbiter (VPO), for remote sensing of the atmospheric, and the Venus Elliptical Orbiter (VEO), which deploys the entry probe from a highly elliptical orbit. The entry probe would contain a balloon-aerobot which floats in benign conditions at 55 km altitude in the middle cloud layer, and would drop up to 15 microprobes into the lower atmosphere.

References

  1. ^ ESA description of the VEP technology reference study
  2. First proposal for launch in 2016-18 timeframe
  3. Second proposal for 2021-23 launch
  4. EVE - European Venus Explorer
  5. ^ Chassefière, E.; Korablev, O.; Imamura, T.; Baines, K. H.; Wilson, C. F.; Titov, D. V.; Aplin, K. L.; Balint, T.; Blamont, J. E. (2009-03-01). "European Venus Explorer (EVE): an in-situ mission to Venus". Experimental Astronomy. 23 (3): 741–760. Bibcode:2009ExA....23..741C. doi:10.1007/s10686-008-9093-x. ISSN 0922-6435.

External links

Spacecraft missions to Venus
Active missions
Orbiters
Flybys


Past missions
Orbiters
Flybys
Descent probes
Landers
Balloon probes
Failed launches
Planned missions
Orbiters
Flybys
Descent probes
Proposed missions
Venus missions
Flybys
Cancelled
or not developed
Program overviews
Related
  • Missions are ordered by launch date. indicates failure en route or before any data returned. indicates use of the planet as a gravity assist en route to another destination.


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