background image

 

 

User’s Manual

 

In Table 1 below, the SFD values are presented for the above mentioned gain settings and for 
each particular satellite antenna. 

 

The quoted figures, based on the less sensitive transponder at nominal configuration, 

represent average values for all transponders. This means that a difference of 1 or 2 dB from 

the specified values is expected. Moreover, the peak gain values correspond to the minimum 
available values. However, the quoted figures can be used in link budget calculations for 

planning  purposes.  
 

A simplified link budget example is presented in Annex A to show how IPFD for saturation is 
employed   in link budget calculations. 

 

Gain 

Step 

F1 antenna 

F2 antenna 

S1 antenna 

S2 antenna 

 Peak 

Gain 

+8.37 dB/K 

Satellite  

Contour 

0 dB/K 

Peak Gain 

+11.10  

dB/K 

Satellite  

Contour 

0 dB/K 

Peak Gain 

+5.94 dB/K 

Satellite  

Contour 

0 dB/K 

Peak Gain 

+5.65 

dB/K 

Satellite 

Contour 

0 dB/K 

5(L) 

-82.20 -73.83 

-84.9  -73.80 

-80.90 -74.96 

-76.80 -71.15 

9(M) 

-88.32 -79.95 

-91.12 -80.02 

-87.16 -81.22 

-82.95 -77.3 

13(H) 

-94.66 -86.29 

-97.37 -86.27 

-93.44 -87.50 

-89.16 -83.51 

Table 1:  Average SFD values for transponder saturation versus sensitivity 

 

Using values from Table 1 and the G/T maps it is easy to calculate the SFD on a specific 
location. The required SFD calculation formula is shown below. 

 
SFD calculation formula:   

 

)

/

/

(

_

L

Peak

Peak

L

Peak

L

T

G

T

G

SFD

SFD

Correction

Aspect

SFD

SFD

+

=

+

=

 

   (Equation 

1) 

 

An appropriate example for the calculation of the SFD and all necessary parameters for a link 
budget can be seen in Annex C.   

 

1.6

 

Β

EACONS 

 

A Ku- band beacon generator on board of the satellite provides a signal   to a dedicated global 

horn antenna. The Ku-band beacon transmits a single right hand circular polarized 
unmodulated frequency of 11.4515 GHz with a maximum EIRP of 12 dBW within the whole 

visible area from the satellite. A 3 dB loss of power level is expected if linear polarization 
reception system is used by the station. This beacon is a two for one redundant unit and is 

used by the earth stations operators to track the Hellas-Sat 2 satellite. 
 

 
 

Summary of Contents for Hellas-Sat 2

Page 1: ...User s Manual H He el ll la as s S Sa at t 2 2 S Sa at te el ll li it te e U US SE ER R s s M MA AN NU UA AL L September 2005 1...

Page 2: ...their systems planning and implementation of satellite services However depending on the case the information and guidance provided cannot be considered as a specification but only as a reference tool...

Page 3: ...ted anywhere over the surface of the visible Earth currently pointing M East S2 and S Africa S1 1 3 FREQUENCY PLAN The frequencies and polarization arrangement of the Hellas Sat 2 satellite transponde...

Page 4: ...by channel basis It is also possible to downlink S2 channels of the 14 25 14 50 GHz band via the F2 antenna in the 11 45 11 70 GHz band but in this case the F2 channels have to be downlinked via the S...

Page 5: ...User s Manual 5 Figure 1 Hellas SAT frequency Plan...

Page 6: ...operation the Camp has 27 gain steps step 0 to 26 with a step size of 1 5 0 3 dB In ALC mode the Camp output signal power is set by telecommand to the required level while the input power may vary ov...

Page 7: ...0 80 90 74 96 76 80 71 15 9 M 88 32 79 95 91 12 80 02 87 16 81 22 82 95 77 3 13 H 94 66 86 29 97 37 86 27 93 44 87 50 89 16 83 51 Table 1 Average SFD values for transponder saturation versus sensitivi...

Page 8: ...arriers for example for 3 carriers there are 9 products and for 5 carriers there are 50 However in most cases only the third order intermodulation products falling within the frequency band of the wan...

Page 9: ...cial coordination and agreement by HELLAS SAT Prior to accessing the Hellas Sat 2 space segment capacity all transmit Earth Station operators have to submit to HELLAS SAT Operations Department Earth S...

Page 10: ...the customer must be ready to go behind specific steps Particularly the Shift Engineer will require the following step by step sequence to be precisely tagged along A CHECK IN 1 Check the antenna reg...

Page 11: ...om Satmaster indicating the required fields needed from the satellite operator G T and EIRP can be extracted from the coverages provided in Annex C G TAthens 6 6dB K EIRPLondon 53dBW SFD can be extrac...

Page 12: ...RP Pattern 8 00 7 00 6 00 5 00 4 00 3 00 2 00 1 00 0 00 1 00 2 00 3 00 4 00 Theta cos phi in Degrees 2 00 4 00 6 00 8 00 10 00 Theta sin phi in Degrees 8 37 8 6 6 6 4 4 4 2 2 2 0 0 0 SATSOFT F1 Horizo...

Page 13: ...00 6 00 4 00 2 00 0 00 2 00 4 00 Theta cos phi in Degrees 2 00 4 00 6 00 8 00 10 00 Theta sin phi in Degrees 11 10 10 8 8 8 8 8 6 6 6 6 4 4 4 2 2 2 2 SATSOFT F2 Horizontal Receive 14 021 MHz G T Patte...

Page 14: ...0 4 00 2 00 0 00 2 00 4 00 Theta cos phi in Degrees 9 00 8 00 7 00 6 00 5 00 4 00 3 00 2 00 1 00 0 00 Theta sin phi in Degrees 5 5 10 10 10 5 94 4 4 4 4 4 2 2 2 2 0 0 0 0 2 2 2 2 SATSOFT S1 Vertical R...

Page 15: ...2 4 4 4 4 6 6 6 6 6 8 8 8 8 8 10 10 10 10 12 12 12 12 14 14 14 14 SAT SOF T S2 Vertical Receive 14 476 MHz G T Pattern 6 00 4 00 2 00 0 00 2 00 4 00 6 00 Theta cos phi in Degrees 1 00 0 00 1 00 2 00 3...

Reviews: