University of Oulu

Space Research GroupCassini project in Oulu

spaceweb@oulu.fi - last update: 20 September 2006 (RR & JV)


Cassini timeline
Launch 15 Oct 1997
1st Venus flyby 26 April 1998
2nd Venus flyby 24 June 1999
Earth flyby 18 August 1999
Jupiter flyby 30 December 2000
Saturn Orbital Insertion (SOI) 1 July 2004
Several Titan flybys 26 October 2004-

Huygens Mission

14 January 2005
Several icy satellites flybys
End of the mission June 2008
Planned extension 2008-2010
Current location
In Finnish - suomenkielinen sivu

NASA satellite CASSINI was launched towards Saturn on 15 October 1997. Cassini arrived to Saturn in summer 2004 and it had an orbital insertion on the 1st of July. Cassini will provide information about the Saturn's magnetosphere, its satellites (especially Titan) and the ring system during the four year official mission. There are also plans for the two year extension of the mission. Titan will be passed several times from the very close distance during the mission as well as the numerous icy satellites of the Saturnian system. The Finnish Meteorological Institute (FMI) has simulated the Titan plasma environment. These simulations will be used when CAPS Titan flyby data is analysed. Also solar wind plasma will be studied at the distance of Saturn while the satellites travel in the solar wind at the far distance from Saturn. Oulu has a co-Investigator status in the CAPS (Cassini Plasma Spectrometer) plasma instrument.

The group has simulated numerically the ion beam spectrometer (IBS) behaviour in order to optimise its properties. The other parts of the CAPS instruments are IMS (ion mass spectrometer) and ELS (electron spectrometer), as shown in the figure below (DPU=Data Processing Unit and ACT = Actuator; click for better resolution).

The IBS instrument is a hemispherical electrostatic analyzer with three fan-shaped entrance windows CAPSfor incoming ions. The angular field of view for each entrance window is 1.5°×150°. Thus angular resolution of the IBS instrument is 1.5°×1.5°. Channel electron multipliers (CEM) are used as detectors. Our simulations shows the energy resolution of the IBS to be 1.4 +- 0.2 %. The deviation comes from minor manufacturing faults: an indentation in the inner hemisphere as well as the misalignment of the hemispheres. The IMS consists of a toroidal electrostatic analyser with following linear electric field time of flight analyser. The ELS is a top hat electrostatic analyser. The IMS and ELS consist of eight separate detectors in 20 sectors. The IMS angular resolution for each detector is 11°×20° and the ELS angular resolution for each detector is 5°×20°. The energy resolution of the ELS is 17%. The energy resolution of the IMS is also 17% and the mass resolution (M/dM) is 80 for particles with energy less than 16 keV/q and 8 for particles with energy more than 16 keV/q.. 

Cassini related papers of the Oulu group

See also

In Finnish - suomenkielinen sivu