4.5m Ring-Focus Antenna, PERFORMANCE SPECIFICATIONS

Model No. SA-4.5TK/C

SPECIFICATIONS

 

C-RECEIVE

C-TRANSMIT

Ku-RECEIVE

Ku-TRANSMIT

 

 

 

 

 

 

Frequency  (GHz)

 

3.7-4.2

5.925~6.425

10.95~12.75

14~14.5

Typical Gain (dBi)

 

43.8

47.2

53

54.5

VSWR

 

1.25:1

1.25:1

1.25:1

1.25:1

Beamwidth:-3dB

 

1.14¡ã

0.72¡ã

0.37

0.31

        -15dB

 

2.4¡ã

1.42¡ã

0.57

0.63

Antenna Noise Temperature (k¡ã)

 

2 Port Feed

 

2 /4 Port  Feed

 

 

 

 

 

 

 

10¡ãElevation

 

36

 

60

 

20¡ãElevation

 

27

 

50

 

40¡ãElevation

 

24

 

44

 

Power Handing Capability

 

 

5 kW/port

 

1kw/port

Feed interface

 

CPR-229G

CPR-159G/137G

 

WR-75

Feed insertion Loss

 

0.25 dB

0.2dB

0.25

0.25

Port-port isolation

 

 

 

 

 

Tx ¨CRx

 

85dB

85dB

 

 

Cross Polarization Isolation (on axis)

 

35dB

35dB

35

35

 

 

 

 

 

 

Axial ratio, dB (Ratio)¡ù

 

1.5dB

1.8dB

 

 

Sidelobes : 

 

CCIR. 580

 

 

 

 

 

 

 

 

 

MECHANICAL SPECIFICATIONS

 

 

 

 

 

Azimuth Travel

 

 

¡À65¡ã

 

 

Elevation Travel

 

 

5¡ãto 90¡ã

 

 

Installation Hardware

 

 

 

 

 

Surface Accuracy

 

 

0.5mm

 

 

Finish

 

 

White paint

 

 

Shipping weight

 

900Kg 

 

 

 

 

 

 

 

 

ENVIRONMENTAL SPECIFICATIONS

 

 

 

 

Operational Winds

 

 

45 mi/h(72km/h) gusts

 

 

 

 

To 60 mi/h (97 km/h)

 

Survival Winds (Any position)

 

 

125 mi/h (200 km/h)

 

Ambient Temperature

 

-45o to 60o

 

Relative Humidity

 

 

0% to 98%

 

Seismic (Survival)

 

 

0.3G´s horizontal,

 

 

 

 

0.15G´s vertical

 

¡ùFor 2-port linear polarization, transmit/receive feed. Polarization is adjustable over a range of 90 degrees with mechanical indicator.

                       4.5m EARTH STATION ANTENNA £¨Ring Focus£©

                        

    We have developed the 4.5 meter C-band and Ku-band antennas with superior performance for receiving only and satellite communication

    transmitting/receiving applications.

The antennas meet the requirements for 2¡ãsatellite spacing per FCC Docket 81-704 and INTELSAT specifications.

Options:

¡ùTwo-port, three-port, four-port Rx/Tx linear or and circular polarized feeds.

¡ùManual or motorization azimuth, elevation and polarization drive systems

               With controls and readouts.


¡¡

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