The
scientific satellite for monitoring the mechanisms of interaction "interplanetary
space-magnetosphere-ionosphere".
Creation of the satellite is planned by the National Space Program for 2008-2012.
The satellite is intended to investigate and predict the space weather (bursts
of solar activity and explosion - like energy releases in the Earth's magnetosphere)
with the aim of ensuring the serviceability of today's technical systems (space
communication, navigation means et al.).
The space weather forecast will allow to solve the following problems in the
vital activity of today's industrial society:
- malfunctions of satellite equipment caused by increased flows of penetrating
radiation and anomalous surface discharges;
- changes of satellite orbits because of atmosphere inflation;
- increase in radiation load on the astronauts and crews of high-altitude aircraft;
- malfunctions and interference in the communication, radar, navigation systems;
- increased interference and spurious currents in the pipelines, cables, electric
power supply lines, railway lines in near-polar latitudes;
- worsening of health of the people with increased sensitivity to external factors
(cardiovascular diseases et al.);
- change of the conditions and characteristics of ionosphere and the Earth's
upper atmosphere, other factor which may have possible impact on the environmental
conditions, ozone layer, climate.
The satellite platform is developed taking into account the today's requirements
to scientific platforms:
- multipoint measurement with the help of identical instruments;
- maximal possible electromagnetic purity of the platform;
- separation of passive and active methods of measurement between different
satellites;
- precise coordinate referencing;
- high information capacity and high rate of telemetry.
Creation of orbital group consisting of several satellites on the same altitude
in one orbital plane is planned on the basis of the platform. Propulsion system
included in the satellite platform allows to form and maintain the spatial structure
of satellite group ensuring effectiveness of scientific experiment performance.
The low-orbit ballistic group of several satellites in combination with the
use of onground means will ensure periodic global nature of measurements.
The set of scientific experiment:
- -a fluxgate magnetometer;
- a Langmuir electric probe;
- an inductive probe;
- a driftmeter;
- a solar photometer;
- a Langmuir probe;
- energy-angular spectrometers;
- a medium energy electrons and protons spectrometer;
- a thermal and super-thermal plasma mass-spectrometer;
- a pulse generator of resonance frequencies;
- a generator of coherent frequencies;
- a receiver of impulse signals of plasma resonance;
- a receiver of coherent frequencies from radio transmission;
- a sensor of high-energy particles;
- an X-ray photometer.
| Initial mass, kg |
270
|
| Mass of scientific equipment, kg |
55
|
| Power consumption of scientific equipment, W |
60
|
| Active lifetime of satellite, years |
3
|
Orbital parameters:
- type of orbit
- altitude, km
- inclination, deg
- local time of descending node longitude
|
sun - synchronous
600-700
~98
direction "morning - evening" (6 hours)
|
| Satellite orientation |
Three axis orbital system of coordinate and passive |
| Satellite orientation accuracy, deg |
1
|
| Angular stabilization rate, deg/s |
0.005
|
| Propulsive mass of propulsion system |
Ammonia
|
| Number of addresses for digital radio commands transmission to scientific
equipment |
not less than 16
|
Number of telemetry inputs:
temperature
analog
signal
potentiometric
|
128
128
512
30
|
| Capacity of onboard memory of the system of scientific data collection,
Gbit |
1
|
| Downlink data rate, kbit/s |
1330
|
|