background image

 

 

User’s Manual

 

1.

 

SATELLITE TECHNICAL CHARACTERISTICS 

 

1.1

 

 INTRODUCTION 

 

This Section contains general information on the multi-region geostationary Hellas-Sat 2 

satellite.  
 

1.2

 

 GENERAL CHARACTERISTICS 

  

The Hellas- Sat 2 satellite is designed for a minimum operational lifetime of 15 years and its 
orbital position can be controlled with ±0.09º East/West and ± 0.05º North/South accuracy 

over at least 12 years. In order to enable the pointing of manually adjusted or program-tracked 
antennas, HELLAS SAT provides, on request, the data for orbit determination to the Earth 

Station operators. Up to thirty (30) transponders of 36 MHz bandwidth each are available for 
simultaneous operation, in eclipse as well as in sunlight. 

Reception and transmission take place via four dual polarized beam antennas. Two of them 
(F1 & F2) are fixed, with a 2.5m main reflector each and dual offset Gregorian configuration of 

single feed with numerically shaped main reflector to provide complex beam shape for efficient 
illumination of Europe, and part of Middle East and N. Africa. The other two antennas (S1&S2) 

also Gregorian, are steerable with a shaped parabolic reflector of 1.3m to provide spot 
coverage and can be pointed 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 transponders are 
shown in Figure 1.  

 
The fixed coverage antenna F1 receives signals in the band 13.75-14.00 GHz whilst the fixed 

coverage antenna F2 receives signals in the band 14.00-14.25 GHz. The steerable antenna S1 
receives signals in the band of 13.75-14.00 GHz. 

The steerable antenna S2 receives signals in the band 14.00-14.25 GHz on the horizontal 
uplink polarization and in band 14.00-14.50 GHz on the vertical uplink polarization. There are 

two types of receivers/downconverters. 
 

Type 1 receiver provides frequency translation of either uplink band 13.75-14.00 GHz or 14.00-
14.25 GHz to downlink band 12.50-12.75 GHz using two switchable local oscillators 

(1.244GHz and 1.5GHz respectively). These receivers are connected in a 8/6 redundancy 
scheme.  

 
Type 2 receiver provides frequency translation of uplink band 14.00 to 14.25GHz, to downlink 

band 10.95 to 11.20 GHz using a 3.050 GHz local oscillator.These receivers are connected in 
a 2/1 redundancy scheme. 

 
There are also two downconverter assemblies that provide frequency translation of the S2 

uplink band 14.25-14.50 GHz to downlink band 11.45 to 11.70 GHz using a 2.8 GHz local 
oscillator and connected in a 2/1 redundancy scheme. 

 

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: