VENUS EXPRESS
Venus Express (VEX) is the second planetary mission for the European Space Agency (ESA) and
is the first mission to Venus for over 15 years. The mission is based on the Mars Express (MEx) and
Rossetta missions to Mars and a cometary body. The spacecraft reuses many components and instruments from
these previous missions.
The main characteristics of VEX are:
- Dimensions: 1.65m x 1.75m x 12.4 m excluding solar pannels. Its size with the solar pannels extended is of 8 m.
- Total mass 1270 kg, 93 kg belong to the scientific instruments and 570 kg are for fuel for inflight maneuvers.
- A main engine and 8 smaller engines for trayectory correction.
- Solar pannels highly reflective to reduce the heating. The electrical power produced by the pannels is of 800 W in Earth orbit and 1370W in Venus orbit.
- High gain antenna of 1.3 m diameter and a secondary lower gain antenna. Connexion time to Earth is of 7 to 10 hours every orbit.
- 12 Gb solid state memory.
- Polar orbit with a period of 24 h and minor distance to Venus of 250 km and largest distance of 66.000 km.
The
scientific instruments onboard VEX are:
- ASPERA-4: (Led by Institute of Space Sciences, Kiruna, Sweden)
"Analyzer of Space Plasmas and Energetic Atoms,"
This instrument will investigate the interaction between the solar wind and the Venusian atmosphere,
determine the impact of plasma processes on the atmosphere, global distribution of plasma
and neutral gas, 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 more energetic environment near-Venus.
See pictures of the ASPERA-4
instrument on the IRF at the Sweedish Institute of Space Science.
- MAG (Led by IWF, Graz, Austria)
This magnetometer will measure the strength of Venus's magnetic field and the direction of it
as affected by the solar wind and Venus itself. It will also aid ASPERA-4 in the study of
the interaction of the solar wind with the atmosphere of Venus. MAG is derived from the Rosetta
lander's ROMAP instrument.
- PFS (Led by IFSI-ISI, Rome, Italy)
The "Planetary Fourier Spectrometer" operates in the infrared between the 0.9 µm and 45 µm wavelength
range and is designed to perform vertical optical sounding of the Venus atmosphere. It will perform global,
long-term monitoring of the three-dimensional temperature field in the lower atmosphere (cloud level up to 100 kilometers).
It will also search for minor atmospheric constituents that may be present, analyze atmospheric aerosols,
and investigate surface to atmosphere exchange processes.
The design is based on a spectrometer on Mars Express, but modified for optimal performance for the Venus Express mission.
Go to the official Venus Express PFS webpage.
- SPICAV
(Led by Service d’Aeronomie du CNRS, Verriesres, France; Institute for Space Aeronomy, Belgium; IKI, Russia)
Short for "Spectroscopy for Investigation of Characteristics of the Atmosphere of Venus",
SPICAV is an imaging spectrometer that will be used for analyzing radiation in the infrared
and ultraviolet wavelengths. In particular, it will search for the small quantities of water
expected to exist in the Venusian atmosphere. It will also look for sulphur compounds and molecular
oxygen in the atmosphere. It will determine the density and temperature of the atmosphere at 80–180
kilometres altitude.
It is derived from the SPICAM instrument flown on Mars Express. However, SPICAV has an additional channel
known as SOIR (Solar Occultation at Infrared) that will be used to observe the Sun through Venus's atmosphere
in the infrared in the occultation experiments planned.
More information (in French only) here.
Pictures can be found here
- VERA:
(Led by Univ. der Bunderswehr, Munich, Germany)
The Venus Radio Science is a radio sounding experiment that will transmit radio waves from the spacecraft
and pass them through the atmosphere or reflect them off the surface. These radio waves will be received
by a ground station on Earth for analysis of the ionosphere, atmosphere and surface of Venus.
Scientists will also use it to study the density, temperature, and pressure of the atmosphere
from 35–40 km up to 100 km from the surface, and to determine roughness and electrical
properties of the surface. It will also allow investigations of the conditions of the solar wind in the inner
part of the Solar System. It is derived from the Radio Science Investigation instrument flown on Rosetta.
- VIRTIS:
(Led by CNR-IASF, Rome, Italy, and Observatoire de Paris, France)
VIRTIS (Visible and Infrared Thermal Imaging Spectrometer) is an imaging spectrometer that observes
in the near-ultraviolet, visible, and infrared parts of the electromagnetic spectrum. It will analyze
all layers of the atmosphere, surface temperature and surface/atmosphere interaction phenomena.
It will obtain point spectra and track the clouds in both ultraviolet and infrared wavelengths
in the day and night side and will allow scientists to study atmospheric dynamics at different altitudes.
More information at the
VIRTIS for Venus Express webpage.
- VMC:
(Led by MPS, Katlenburg-Lindau, Germany)
The Venus Monitoring Camera is a wide-angle, multi-channel CCD.
It will be able to make global images and will study the cloud dynamics and image the surface.
It will also assist in the identification of phenomena seen by other instruments.
VMC will operate in the visible, ultraviolet, and near infrared spectral ranges. It will map surface brightness distribution and search
for volcanic activity, monitor airglow, study distribution of unknown ultraviolet absorbing phenomenon
at the cloud-tops, and other science observations. It will create images and movies as well.
It is a new instrument derived only in part by the Mars Express High Resolution Stereo Camera (HRSC)
and the Rosetta Optical, Spectroscopic and Infrared Remote Imaging System (OSIRIS).
More information at the VMC for Venus Express
webpage at the Max Planck Institute for Solar System Research.