On-the-move satellite communications antenna system was developed for the emergency communication application. It suit for moving carriers. The field of application is public security, civil air defense, and so on.
Technical specfication
RF characteristic | |||||||||
size |
0.6m |
0.8m |
0.9m |
1.2m | |||||
Frequency |
Rx(GHz) |
12.25~12.75 | |||||||
Tx(GHz) |
14.0~14.5 | ||||||||
Gain |
Rx(dB) |
32.9 |
37.5 |
38.9 |
41.2 | ||||
Tx(dB) |
36.5 |
38.7 |
40.2 |
42.5 | |||||
G/T (11.7GHz, 20EL 70LNA)dB/k |
14.1 |
16.8 |
17.8 |
20.4 | |||||
Interface |
WR-75 | ||||||||
Wave width |
Rx |
2.95 |
2.2 |
1.9 |
1.45 | ||||
Tx |
2.5 |
1.9 |
1.6 |
1.25 | |||||
Sidelobes characteristic |
CCIR580-4/ITU | ||||||||
Standing wave ratio |
Rx |
1.25 | |||||||
Tx |
1.25 | ||||||||
Cross Pol: |
85 dB | ||||||||
Power Capacity |
1 KW | ||||||||
Polarizations |
level,upright | ||||||||
Cross Pol differentiate |
≥35dB ( axis); ≥30dB (1 dB Wave width) | ||||||||
Mechanical characteristic | |||||||||
High |
570mm |
918mm |
969mm |
1121mm | |||||
Radome |
780mm |
φ910 mm |
1012 mm |
1316 mm | |||||
Base dia. |
410mm |
φ470 mm |
470 mm |
470 mm | |||||
Weight |
47 Kg |
90 Kg |
90 Kg |
90 Kg | |||||
Speed |
150 Km/h (Max) | ||||||||
Power Supply |
210V~240V AC, 50/60Hz | ||||||||
Power(Max) |
650W (Max) | ||||||||
Temperature |
-25℃~+45℃ | ||||||||
Humidity |
100% | ||||||||
Tracking characteristic | |||||||||
Position Scope |
360 no limitation |
360 no limitation |
360 no limitation |
360 no limitation | |||||
Pitching |
5~95 | ||||||||
Polarazition |
185 | ||||||||
Azimuth Speed(Max) |
100/S |
100/S |
100/S |
100/S | |||||
Azimuth Acceleration Speed(Max) |
1100/S2 |
60/S2 |
60/S2 |
600/S2 | |||||
Pitch angle speed(Max) |
80/S |
60/S |
60/S |
60/S | |||||
Pitch angle Acceleration speed(Max) |
750/S2 |
600/S2 |
600/S2 |
600/S2 | |||||
Tracking Accuracy |
Cross-country road:signal tracking loss ≤1dB(RMS) | ||||||||
Flatness road:signal tracking loss ≤0.2dB(RMS) | |||||||||
Capture satellite time |
<3 Sec(preliminary);<1 Sec(re-capture time) |