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The
6 kg Munin nanosatellite is sponsored by the Institutet för RymdFysik (Swedish Institute of
Space Physics), Umeå
University, and Luleå University of Technology. The scientific objective is to collect data on the
auroral activity for both the northern and southern hemispheres,
such that a global picture of the current state of activity can be
made available on-line. The data acquired by Munin will then serve
as an input to the prediction of space weather.
The
satellite uses a passive magnetic stabilization system, a
permanent magnet holds the satellite aligned along the geomagnetic
field lines (like a compass needle). The satellite has no moving
parts, deployable booms, etc. The stowed dimension of the
satellite is 20 x 20 x 25 cm. The satellite is
covered with solar cells on all surfaces. The satellite is powered
by the solar cells, which provide enough power when the satellite
is in sunlight to also recharge a battery that will keep the
satellite powered when it is in eclipse.

Munin was placed
in an elliptical orbit, 698 x 1810 km (377 x 977 nmi), at 95.4
degrees inclination. In the orbit it collects
information about the distributions of electrons and ions and
stores this in the onboard (2Mb) RAM. By using artificial intelligence and compression methods we can be
sure of only storing interesting data. This data is downlinked
with use of a radio modem when the satellite passes Kiruna,
Sweden, and will be made available on the world wide web
immediately after reception.

The
name of the satellite comes from Nordic mythology: "The
ravens Munin and Hugin flew out and brought back news from every
corner of the world. Sitting on the God Odin's shoulders, they
whispered all the news in his ears. Munin represented the memory
and Hugin the intelligence... and they were his embodied
soul..."
| Munin
|
|
SATELLITE
|
| Int'l Designation |
2000
075C
|
Launched
|
| Owner / Sponsor |
Institutet för RymdFysik (Swedish Institute of
Space Physics)
|
| Mission |
Science
|
| Satellite Bus |
custom
|
-
|
| Launch Mass |
6
kg (13.25 lbm)
|
| Mission Orbit |
LEO /
698 x 1810 km (377 x 977 nmi)
|
95.4°
|
| Design Life |
|
| Power (EOL) |
|
|
LAUNCH
|
| Launch Vehicle
Model |
Delta
2 7320-10 |
| Launch Date / Time |
2000
Nov 21
|
18:24:25
|
| Co-Passenger(s) |
EO
1 |
| |
SAC
C |
|
Financial
|
| Satellite cost |
|
| Web Links |
Munin
Web Site
|
|