SWAN Instrument

Description

The instrument is equiped with two identical sensor units pointing the northern and southern ecliptic hemispheres respectively. The field of view (FOV) of each sensor is of 5° x 5° divided on 5 x 5 pixels of 1° square each. The sensor is completed by a mechanical periscope system containing two mirrors at 45° incidence. The moving mirror system allows full sky mapping in Ly-α.

SWAN sensor unit scheme

A hydrogen cell is placed in each sensor's optical path, which provides quantitative information on the spectral profile of the Ly-α line, with a resolving power of about 3 x105. The cell contains molecular hydrogen at few hundreds of Pascals pressure, dissociated by two heated tungsten filaments. When the cell is activated, hydrogen atoms, produced by the dissociation process, absorb in resonance the Ly-α line emitted by interplanetary (IP) hydrogen atoms.

SWAN Characteristics

Total Mass13.25 kg
Mass of Electronic Unit2.82 kg
Mass of one Sensor Unit4.815 kg
Average Power11 W
Telemetry200 bps
Telecommands69 different TC
Working Temperature0 to +30° C
Overall FOVmore than 2π sr for each sensor unit (2-mirror periscope)
Instantaneous FOV25 pxls of 1° x 1° = 5° x 5°
Wavelength range115 - 180 nm
Photometric Sensitivity0.75 counts /sec /Rayleigh /1° pxl
Type of detectorSolar blind MgF2 / CsI Cathode - Multianode MCP
Expected count ratefrom 200/s (IP) to 104 /s (solar corona) per pixel
Relative accuracybetter than 1% for 45 sec counting time on IP signal
Absolute sensitivitychecked at regular time intervals with stellar calibrations
Hydrogen cellPyrex vessel (MgF2 lens windows-distance 76mm)
Spectral Resolution : better than 0.01Å (Resolving power 105)

see also FMI SWAN pages

Last updated on Mon, Feb 7, 2005 DK