AlfaRadio AlfaSpid Rotator and Controller Instrukcja Użytkownika Strona 2

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S-band ground station prototype for low-earth orbit nanosatellite missions
TELECOMUNICAŢII Anul LII, nr. 2/2009 65
2. Space communication system
architecture
The simplified space communication system ar-
chitecture, presented in Fig. 2.1, is splited into two
physically separated units: the nanosatellite trans-
ceiver and the ground station. The nanosatellite and
the ground station can communicate via a circular
polarized (LHCP/RHCP) link operating in some S-
band portion allocated to Earth-space communica-
tions or to amateur radio service. The ground station
has a modular architecture in order to meet different
communication requirements which are application
dependent. The station main sub-systems are:
the elevation-azimuth motorized antenna;
a radio unit (satellite or application dependent);
the satellite tracking module;
a GPS module for time synchronization;
the TLE data update module.
3. Ground station prototype
implementation
Most of the components which are integrated in
sub-systems are commercial off-the-shelf radio hard-
ware and software. The components were selected to
meet the requirements imposed by the uplink and
downlink budgets for the first Romanian nanosatellite.
3.1. Elevation & Azimuth motorized antenna
sub-system
The ground antenna consists of a radio amateur
highly directional 3M (F/D= 0.4 ratio) parabolic mesh
dish antenna. The operating range of the antenna is
from 1 to 6 GHz and has 65% efficiency. The gain at
2400 MHz is more than 35 dBd and the -3dB beam
width is approximately 2.9°. The mesh minimizes
problems with wind loading on the mounting hard-
ware caused by periodic local windstorms. For dish
specifications – see Table 3.1.
Table 3.1
The 3 meter mesh dish specifications
(Efficiency 65%)
Frequency Gain [dBd] -3dB angle (degrees)
1296 MHz 30.3 5.7
2320 MHz 35.4 3.2
3456 MHz 38.8 2.1
5760 MHz 43.3 1.3
Weight 40 kg
Fig. 2.1. Basic Architecture of the S-Band Space Communication System.
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