| LINK BUDGET CALCULATION FOR EMWIN-N | |||||
| Parameter | Units | Value | |||
| Data Rate | bps | 9600 | |||
| Modulation Type | BPSK | ||||
| FEC Coding Type | Conv+RS | ||||
| FEC Coding Rate | 0.437 | ||||
| Ground Uplink Transmitter | |||||
| Uplink Frequency | MHz | 2034.70 | |||
| Transmit EIRP | dBmi | 76.7 | |||
| Antenna Pointing Loss | dB | 0.5 | |||
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| Earth - To - Space | |||||
| Path Distance (for 5 deg elevation) | km | 41127 | |||
| Free Space Loss | dB | 190.9 | |||
| Atmospheric Attenuation | dB | 0.4 | |||
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| S/C Receive Performance | |||||
| Polarization Loss | dB | 0.2 | |||
| U/L Incident Power | dBmi | -115.3 | |||
| Antenna Gain (from 5 deg elevation) | dBi | 14.8 | |||
| G/T (incl cable losses) | dB/K | -14.2 | |||
| Boltzmann constant | dBm/Hz/K | -198.6 | |||
| Uplink Thermal C/No | dB/Hz | 69.1 | |||
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| S/C Transmit Performance | |||||
| Downlink Frequency | MHz | 1692.70 | |||
| Transmit EIRP (to 5 deg elevation) | dBmi | 44.8 | |||
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| Space - To - Earth | |||||
| Path Distance (for 5 deg elevation) | km | 41127 | |||
| Free Space Loss | dB | 189.3 | |||
| Atmospheric Attenuation | dB | 0.4 | |||
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| Ground Downlink Receiver | |||||
| Downlink Incident Power | dBmi | -144.90 | |||
| Pwr Flux Density Rqmt (EOC in 4 kHz) | dBW/m2 | -154 | |||
| Power Flux Density (EOC in 4 kHz) | dBW/m2 | -156.9 | |||
| E/S G/T | dB/K | -0.3 | |||
| Polarization Loss | dB | 0.2 | |||
| Boltzmann constant | dBm/Hz/K | -198.6 | |||
| Downlink Thermal C/No | dB/Hz | 53.2 | |||
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| Eb/No Overall Calculation | |||||
| Overall Composite C/No | dB/Hz | 53.1 | |||
| Data Rate in dB | dB-Hz | 39.8 | |||
| Eb/No Calculated | dB | 13.3 | |||
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| Required Eb/No Adjustments | |||||
| Required BER | 1E-06 | ||||
| Theoretical Eb/No | dB | 2.6 | |||
| Ground Segment Implementation Loss | dB | 2.0 | |||
| Satellite Segment Degradations | dB | 1.0 | |||
| Required Eb/No | dB | 5.6 | |||
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| Eb/No MARGIN | dB | 7.7 | |||
Some specific points for consideration:
1. The downlink power used is the 44.8 dBmi minimum.
2. The Implementation Loss of 2.0 dB is based on the performance demonstrated by
the Avtec
prototype.
3. The Satellite Segment Degradations value of 1.0 dB is an estimation. Its true
value will not be known
until an actual test is made through the GOES N or O transponder.
4. The bottom line margin is relatively high, but may be reduced due to items 2
and 3 above. In
addition, the steep curve of BER v. Eb/No for the FEC coding used, makes the
coded link more vulnerable to
interference than a non-coded link, so some of this margin should be reserved to
decrease this vulnerability. (2 dB is
recommend.)