background image

 

 

User’s Manual

 

1.7

 

TWTA TRANSFER CHARACTERISTICS 

 

All TWTA which are employed on Hellas- Sat 2 transponders provide a maximum output power 
of 105W. 

The OBO denotes the power level available at the output of the TWTA relative to that when the 

transponder is saturated. The OBO is therefore very important for link budget calculations as it 
provides the available power per carrier for one or more carriers in the down link. 

 
Operation of the TWTA at saturation means that the maximum output power is obtained in the 

down link which in turn directly affects the design of the terrestrial receive equipment. 
   

When a number of  carriers are simultaneously amplified at different frequencies  by the power 
amplifier of a satellite transponder  or of  a transmit E/S, non-linearities of the amplifiers cause 

intermodulation, i.e produce unwanted signals, called intermodulation products.  
 

The number of intermodulation products increases very quickly with the number of input 
carriers (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 wanted carriers are considered.  

 
To reduce intermodulation products in multicarrier operation (FDMA mode) the TWTA needs to 

be driven with a sufficient back-off:  i.e an input back-off of about 9 dB corresponding to an 
output back-off of about 4.1 dB. In the case of earth station HPAs, an output back-off is usually 

required (3 to 8 dB). However the situation can be improved by the utilization of linearizers. 
Above limitations do not apply in the case of a single carrier occupying the whole transponder 

bandwidth and therefore the TWTA can be driven almost to saturation.    
For a Hellas-Sat 2 TWTA, in different operational modes, the following total IBO/OBO values 

may be employed: 
 

  

  

No of Carriers 

  

MultiCarrier 

IBO 

0 -5 -7.5 -7 

-9 

OBO 

0 -2 -3.1 

-3.9 

-4.1 

Trp 1-12,  

Beams F2, S2 

C/IM 

- 27.7 18.5 18 

18 

  

  

No of Carriers 

  

MultiCarrier 

IBO 

0 -5 -8.5 -8 

-10.5 

OBO 

0 -2 -3.5 

-3.4 

-4.9 

Trp 13-24 & 25-48  

Beams F1, S1, S2/F1 

C/IM 

- 26.5 18  18 

18 

Table 2:  IBO vs. OBO for multi-carrier operation 

                                                     

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: