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TELE-X - a Satellite System for TV and Data Communication ...

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Fig. 5<br />

Block diagram of the payload with its transponder<br />

<strong>and</strong> antenna systems<br />

<strong>Data</strong> <strong>and</strong> video transponders (upper half of the<br />

diagram)<br />

The signal received from the antenna is preamplified<br />

<strong>and</strong> frequency shifted in one of two<br />

receivers (redundancy). The signals are filtered<br />

<strong>and</strong> divided between a wideb<strong>and</strong> <strong>and</strong> a narrowb<strong>and</strong><br />

transponder. The subsequent amplification<br />

takes place separately at 12 GHz <strong>and</strong> uses a<br />

common st<strong>and</strong>by channel. The final amplification<br />

takes place in travelling wave tubes of the same<br />

type as the <strong>TV</strong> tubes <strong>and</strong> with the same saturation<br />

power, 220 W. However, the operating point used<br />

<strong>for</strong> the TWTs is approximately 7dB lower than <strong>for</strong><br />

the <strong>TV</strong> tubes, which gives a linear characteristic<br />

with an output power of approximately 45 W.<br />

Additional improvement of the linearity is obtained<br />

by means of amplitude <strong>and</strong> phase correction<br />

in a linearity unit placed be<strong>for</strong>e the final<br />

amplifiers. This is necessary in order to avoid<br />

intermodulation (crosstalk) between the many<br />

carriers in the transponder.<br />

<strong>TV</strong> transponder (lower half of the diagram)<br />

The incoming signal is amplified <strong>and</strong> frequency<br />

shifted, <strong>and</strong> then divided between the three <strong>TV</strong><br />

channels 26, 32 <strong>and</strong> 40 according to the WARC<br />

plan. The final amplification is provided by travelling<br />

wave tubes, which increase the total amplification<br />

to 220 W. Because of the restricted power<br />

supply only two of the three channels are normally<br />

used. All <strong>TV</strong>, data <strong>and</strong> video transponder<br />

signals are combined in a filter at the output <strong>and</strong><br />

fed out to the common transmit antenna. Like the<br />

separate receive antenna this is a Cassegrain<br />

antenna with a half power lobe width of 1.6x0.8 .<br />

The system also contains a receiver ("RF sensing")<br />

which senses the transmission direction to<br />

the control station on the ground. The antenna<br />

can thereby be directed towards the desired point<br />

<strong>and</strong> kept to within 0.05 .<br />

Ericsson Radio <strong>System</strong>s isthe main supplier<br />

of the FLS station The Finnish<br />

company Valmet OY <strong>and</strong> the National<br />

Finnish Technical Research Centre supply<br />

the antenna.<br />

The space segment<br />

The <strong>TELE</strong>-X satellite will be launched by<br />

an ARIANE rocket in February 1987 <strong>and</strong><br />

placed in a geostationary orbit at a longitude<br />

of 5 C east.<br />

The satellite consists of two main parts,<br />

the payload <strong>and</strong> the plat<strong>for</strong>m The payload<br />

consists of the communication<br />

equipment on board.<br />

The plat<strong>for</strong>m includes functions <strong>for</strong> propulsion,<br />

attitude <strong>and</strong> orbit control,<br />

power supply, temperature regulation<br />

<strong>and</strong> also telemetry <strong>and</strong> comm<strong>and</strong>. The<br />

plat<strong>for</strong>m is almost identical to those<br />

used in the German <strong>and</strong> French <strong>TV</strong> satellites<br />

<strong>TV</strong>-SAT <strong>and</strong> TDF-1. They have all<br />

been produced by the same group of<br />

companies (mainly Aerospatiale <strong>and</strong><br />

Thomson-CSF, France, MBB <strong>and</strong> AEG-<br />

Telefunken, West Germany, <strong>and</strong> Ericsson<br />

Radio <strong>System</strong>s <strong>and</strong> Saab Space,<br />

Sweden). However, the Swedish share<br />

of the production is much greater in<br />

<strong>TELE</strong>-X than in the French <strong>and</strong> German<br />

satellites.<br />

The plat<strong>for</strong>m parts are being tested <strong>and</strong><br />

space qualified in the French-German<br />

projects, whose time plans are approximately<br />

one year ahead of <strong>TELE</strong>-X. The<br />

payload is to a great extent new, but as<br />

far as possible it has been based on previous<br />

experience.<br />

FA<br />

D/V-RCVR<br />

IMUX<br />

NB<br />

WB<br />

SW<br />

GCA<br />

TWT<br />

CA<br />

OMUX<br />

<strong>TV</strong>-BSU<br />

Antenna feeder<br />

<strong>Data</strong>/Video receiver (with redundancy)<br />

Input filter<br />

Narrow-b<strong>and</strong> channel <strong>for</strong> 40 MHz<br />

Wideb<strong>and</strong> channel <strong>for</strong> 85 MHz<br />

Switch<br />

Channel amplifier with linearizer<br />

Travelling wave tube<br />

<strong>TV</strong> channel amplifier<br />

Output filter<br />

Wide-b<strong>and</strong> preamplifier (with reduncancy)<br />

Fig. 6<br />

The division of traffic between the data <strong>and</strong> video<br />

channels in <strong>TELE</strong>-X.<br />

The earth stations are designed so that traffic at<br />

34 Mbit s <strong>and</strong> 8 Mbit s is transmitted in the wideb<strong>and</strong><br />

transponder (WBT). WBT is designed to<br />

h<strong>and</strong>le data rates of up to 140Mbit/s.<br />

The 64kbit/s transmission takes place via the<br />

narrow-b<strong>and</strong> transponder (NBT), which can take<br />

500 simultaneous carriers (channels).<br />

2 Mbit/s traffic can be transmitted in either WBT or<br />

NBT. WBT can take 25 channels <strong>and</strong> NBT 20.<br />

Transmitting 2 Mbit/s traffic via NBT reduces the<br />

number of available 64kbit/s channels. Each<br />

2 Mbit/s carrier occupies the same frequency<br />

b<strong>and</strong>width as 25 different 64kbit/s channels

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