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SATELLITE EARTH STATION ANTENNA By Naveen Jakhar, ITS
31

Presentation on satellite antenna

Feb 14, 2017

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Page 1: Presentation on satellite antenna

SATELLITE

EARTH STATION ANTENNA

By Naveen Jakhar, ITS

Page 2: Presentation on satellite antenna

FREQUENCY BANDS

1. VLF 10-30 KHz World wide Telegraphy

2. LF 30-300 KHz Marine & Navigation

3. MF 300-3000 KHz MW & SW Broad-

4. HF 3-30 MHz Casting

5. VHF 30-300 MHz MARR, TV Radar,

Aeroplane, Navigation

6. UHF 300-3000 MHz TV, UHF

7. SHF 3-30 GHz Microwave & Satellite

(Super High Freq.)

8. EHF 30-300 GHz Experimental

(Extremey High Freq.)

Page 3: Presentation on satellite antenna

High Gain

Wide Band width

Low Noise Temp.

Massive size.

Complete Steer ability in X-Y plane.

Narrow beam width,

Low side Lobes &

High polarization discriminations.

Satellite Earth Station Antenna characteristics.

Page 4: Presentation on satellite antenna

Noise Figure, F = SNRin / SNRout

F = Si /Ni = No = No …….So/No (So/Si) Ni G Ni

F = GNi + Na = 1 + Na GNi GNi GNi is the out put noise power of a noise free network.

The value of F is standardized by fixing the input noise power as that produced by a matched source at a standard temperature of 290 K (17 C).

A noise less network has a noise figure of unity. Real networks always have a noise figure greater than

unity.

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Si, NiSo, No

F

G

Page 5: Presentation on satellite antenna

The total noise in the receive chain (at the input of

demodulator) may be expressed in the form of noise

temperature.

Pn = k . Te . B

Where,

Pn = Generated noise power

k = Boltzman’s constant

= 1.38x 10exp(-23) Joules/K

B = Bandwidth over which noise is generated.

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Page 6: Presentation on satellite antenna

Noise Figure, F = 1 + Na / G Ni

Na= Noise added by the Amplifier

F = 1 + G k Te B / G k To B

To is 290 K (17 degree C)

Or, F = 1 + Te / To

Or, Te / To = F – 1

Or, Te = To ( F – 1)

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Page 7: Presentation on satellite antenna

Noise Figure in db = 10 log10 ( 1 + Tn /290

)

For an amplifier of Tn = 865 K

Noise Figure = 10 log10 ( 1 + 865/ 290)

= 10 (0.6) = 6 db

Noise Figure = 10 log10 ( Noise Factor)

6 db = 10 log10 ( Noise Factor)

Noise Factor = 4

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Page 8: Presentation on satellite antenna

Low Noise Temperature :

High performance is required because signal levels to be

handled by the antenna are very-very low .

C/N requirement (Noise is very important factor)

Noise added by the antenna should be as low as possible.

Noise sources :

Sky Noise Collected by the antenna aperture.

Feed (Most important Noise Contributor) even 0.1 dB noise

addition affects noise temperature appreciably.

Wide Band Characteristics :

Antenna System should have sufficient band width.

So that performance is not affected.

Polarizer & Duplexer should be designed specifically.

Page 9: Presentation on satellite antenna

Narrow beam width

Mechanical Characteristics :

High mechanical accuracy.

Tracking accuracy within 1/10th of beam width.

High surface Accuracy.

Steer-ability (should be track-able to all possible satellite

locations).

Page 10: Presentation on satellite antenna

Classification of Antenna

(a) Radiation System. & (b) Mount Structure.

(a) Radiation System :-

(i) Horn Reflector Antenna

- Developed by Bell labs USA for satellite communication

- High Radiation efficiency.

- Good Noise Temperature performance.

It is very expensive because of its too huge structure in

proportion to its effective antenna aperture.

Page 11: Presentation on satellite antenna

(ii) Parabolic Antenna with Prime Focal Feed :

• Widely used with terrestrial microwave radio relay

links.

• It has high noise temperature characteristics. So

can not be . considered as standard antenna for

Satellite com. (high

noise temp. because of spillover power from main

reflector).

• Long wave guide to connect prime radiator with

LNA.

• LNA can not be mount with the focal feed.

• Mechanical Complexity with the rotating

structure.

• Maintenance problems.

Page 12: Presentation on satellite antenna

(iii) Cassegrain Antenna

- Standard antenna for satellite communication & used

universally.

- Main reflector – parabolic

Sub reflector – hyperboloid

- One of the focii of hyperboloid coincides with focal point

of parabola.

- Other focal point of hyperboloid coincides with phase

centre of primary radiator which is at vertex of paraboloid.

Page 13: Presentation on satellite antenna

Paraboloid primary

reflector

Feed antenna

(horn)

Waveguide

Obstructed ray

Focus of paraboloid

and hyperboloid

Hyperboloid

secondary reflector

Geometry of the Cassegrain feed

Page 14: Presentation on satellite antenna

Cassegrain Feed Antenna

Page 15: Presentation on satellite antenna

Advantages. :-

- Reduction in feed length.

- Ease in Azimuth & elevation rotation along with

antenna structure.

- LNA can be mount very near to primary radiator.

- Low noise temperature.

- High directivity.

- Narrow beam width.

- Feed horn is covered with radomes of glass re-inforced

Teflon sheet.

- Pressurized internally by dry air to prevent moisture.

Page 16: Presentation on satellite antenna
Page 17: Presentation on satellite antenna

Parabolic

SectionCollimate

rays

Axis

Horn

feedFocus

Offset paraboloid reflector

Page 18: Presentation on satellite antenna

Classification based upon

mount structure :

(a) Azimuth Elevation Mount :-

- Primary axis (Azimuth Axis)

is set vertical to the ground.

- Secondary axis (Elevation

Axis) is set Horizontal to the

ground.

- AZ-EL mounting is used

almost universally.

Page 19: Presentation on satellite antenna
Page 20: Presentation on satellite antenna

(b) X-Y Mount :-

- Primary Axis (X-Axis) is

kept parallel to ground such

that antenna dish centre

moves back & forth while

rotation around X-Axis.

- Rotation around Y-Axis

produces both Azimuth &

Elevation Change.

- This mounting is suitable

for small size antenna.

Page 21: Presentation on satellite antenna
Page 22: Presentation on satellite antenna

(c) Polar Mount :

- Here one axis i.e. Ha axis of

the structure is parallel to

the earth’s axis of rotation.

While other axis (Dec.) is

perpendicular to it.

- Tracking is achieved by

rotation around Ha-axis only.

Page 23: Presentation on satellite antenna

(d)Tripod Mount :-

- Suitable for small earth stations.

- Antenna is fixed to a support by three legs.

- Length of one leg is fixed while the other two are variable.

- Limited variations of pointing are possible.

Page 24: Presentation on satellite antenna
Page 25: Presentation on satellite antenna

Antenna being used :

Following type of antenna with Cassegrain structure

are being used.

(i) 11m dia antenna.

(ii) 7.5 m dia antenna.

(iii) 4.5 m dia antenna.

(iv) 3.3 m dia antenna.

(v) 2.4 m dia antenna.

(vi) 8.1 Meter Ku-Band Hub Antenna

Page 26: Presentation on satellite antenna

(i) 11 m dia antenna :-

- Used at Main earth stations,

G/T is 31.7 db/K & 40K LNA.

- Mount structure is Azimuth Elevation type.

- LNAs are mounted inside the centre Hub.

Page 27: Presentation on satellite antenna

(ii) 7.5 m dia Antenna :-

- Used at primary E/S.

- G/T is 25.7 dB/0K and 900K LNA.

- Limited steerability.

(iii) 4.5 m dia antenna :-

- Used at remote E/S.

- G/T is 19.7 dB/0K & 1200K LNA.

- X-Y type mount.

Page 28: Presentation on satellite antenna

- 3.3 m dia Antenna are used for ECTs.

- 2.4 m dia Antenna are used for MCPC-VSAT

stations.

- 14 m dia Antenna is used at MCF Hasan.

- 30 m dia Antenna at VSNL E/S Dehradun.

Page 29: Presentation on satellite antenna

8.1 Meter Ku-Band Hub Antenna

• Antenna

– Parabolic

• Size

– 8.1 Meter

• Feed

– Cassegrene (4 port KU-Band Horn Feed)

• Gain

– 57 dB (Rx)

– 59 dB (Tx)

• Movement

– AZ/EL

• Tracking Mode

– Auto or Manual

• LNA Gain

– 50 dB

• Band Width

– 2050 Mhz

Page 30: Presentation on satellite antenna

1.2 Meter Antenna

Page 31: Presentation on satellite antenna

Thanks.