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User’s Manual

 

 

1.4

 

COVERAGE MAPS 

 
Hellas–Sat 2 satellite provides four antennas for reception. The fixed coverage F1 and F2 

antennas differ only in the shaping of the main reflectors. In practice they provide almost the 

same coverage over Europe, N.Africa and Middle East. 
 

Annex C provides the receive coverage areas in terms of G/T contours for F1, F2, S1 and S2. 
 

The steerable antennas S1 and S2 are currently pointed to cover S.Africa and M.East/Eastern 
Europe region respectively. S1 and S2 are of identical design. 

 
Hellas- Sat 2 provides four antennas for transmission. The fixed transmit coverage of F1 and 

F2 as well as those of the S1 and S2 are presented in Annex C in terms of EIRP contours. 
 

1.5

 

 TRANSPONDER GAIN ADJUSTMENT 

 

Each transponder can be adjusted in terms of its gain. The adjustment is performed by a 
channel amplifier (Camp) which is located before the TWTA. The Hellas- Sat 2 payload has 38 

channel amplifiers. The Camp is a variable gain preamplifier for each individual TWTA and its 
prime function is to limit the effects of rain fade. The Camp can be operated in two modes 

selectable by ground command; Fixed Gain Mode (FGM) and Automatic Level Control (ALC) 
mode.  

In FGM, the gain of the Camp is selectable by telecommand. In this mode of 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 over a specified dynamic range. In this mode of operation the Camp 
has 17 gain steps (0-16), with a step size of 1±0.25 dB 

 

From the operational point of view, the above arrangement provides flexibility to the earth 

station operators in cases where the uplink station is power-limited and/or where power 
compensation is required to cater for unpredictable link fade (rain etc.).  

 

1.5.1

 

Saturation Flux Density (SFD) 

 

The input power flux density for saturation of each channel is calculated at peak satellite 

antenna gain. The peak saturated flux density is used in relation with the antenna G/T contours 
relative to peak antenna gain and the sensitivity (gain step) of the transponder. The sensitivity 

of each transponder may be adjusted independently from the others. 
 

The SFD for transponder saturation at peak satellite antenna gain (at the maximum satellite 
G/T point) ranges from  about – 75  to – 115dBW/m² depending on the transponder gain step, 

the antenna each transponder is connected to, and  the particular TWTA. 
 

Operationally, three gain modes are used; Low (L), Medium (M) and High (H). However, there 
is the possibility to use other gain steps depending on the earth station EIRP capability, the 

receive earth station G/T, earth stations location, the desired quality etc. 
   

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...

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