2.4m Ring-Focus Antenna, PERFORMANCE SPECIFICATIONS

Model No.SA-2.4TK/C

SPECIFICATIONS

 

C-RECEIVE

C-TRANSMIT

Ku-RECEIVE

Ku-TRANSMIT

 

 

 

 

 

 

Frequency  (GHz)

 

3.625-4.2

5.85~6.425

10.95~12.75

14~14.5

Typical Gain (dBi)

 

35.8

39.5

47.5

49

VSWR

 

1.25:1

1.25:1

1.25:1

1.25:1

Beamwidth:-3dB

 

2.87¡ã

1.92¡ã

0.48

0.34

        -15dB

 

5.96¡ã

3.86¡ã

0.97

0£®68

Antenna Noise Temperature (k¡ã)

 

2 Port Feed

 

2 Port Feed

 

 

 

 

 

 

 

10¡ãElevation

 

41¡ãk

 

52

 

20¡ãElevation

 

35¡ãk

 

44

 

40¡ãElevation

 

35¡ãk

 

38

 

Power Handing Capability

 

 

5 kw/port

 

1kw/port

Feed interface

 

CPR-229G

CPR-159G

 

WR-75

Feed insertion Loss

 

0.15  dB

0.18dB

0.4

0.4

Port-port isolation

 

 

 

 

 

Tx ¨CRx

 

85dB

 

 

 

Cross Polarization Isolation (on axis)

 

35dB

35dB

35

35

 

 

 

 

 

 

Axial ratio, dB (Ratio)¡ù

 

0.5

0.5

 

 

Sidelobes : 

 

CCIR. 580

 

 

 

 

 

 

 

 

 

MECHANICAL SPECIFICATIONS

 

 

 

 

 

Azimuth Travel

 

¡À90º

 

 

 

Elevation Travel

 

50   to 90o

 

 

 

Installation Hardware

 

 

 

 

 

Shipping weight

 

280kg

 

 

 

Surface Accuracy

 

0.5mm

 

 

 

Finish

White paint

 

 

 

 

 

 

 

 

 

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

 

-30o to 60o

 

 

Relative Humidity

 

0% to 100%

 

 

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.

 

                       2.4m EARTH STATION ANTENNA £¨Ring Focus£©

                         

We have developed the 2.4 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.

     Manual azimuth, elevation and polarization drive systems.


¡¡

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