
Link Budget calculations.
Path Loss Formula L(dB) =32.45 +20 log F(MHz) +20 log D(Km)
maximum distance for 800 Km polar orbit 3000 Kms
minimum distance for orbit 800 Kms
Downlink:
Maximum path loss at 29 MHz = 131.24 dB
Maximum path loss at 146 MHz = 145.28 dB
Maximum path loss at 435 MHz = 154.73 dB
Maximum path loss at 2400 MHz = 169.59 dB
Assume spacecraft antenna gain of 0 dBi, 1 watt transmitter power,
and the following net antenna gains for the ground station:
29 MHz = 0 dBi
146 MHz = 6 dBi
435 MHz = 9 dBi
2400 MHz = 15 dBi
we obtain the received signals at maximum range as follows:
29 MHz = -101.24 dBm
146 MHz = -109.28 dBm
435 MHz = -115.73 dBm
2400 MHz = -124.59 dBm
So 29 MHz, 146 MHz, or 435 MHz will provide a workable downlink signal.
Doppler shift:
Taken from "The Satellite Experimenters Handbook" table 13-1 page 13-5.
29 MHz = 0.70 KHz
146 MHz = 3.45 KHz
435 MHz = 10.3 KHz
2400 MHz = 56.7 KHz
So 29 MHz, 146 MHz, or 435 MHz will provide a workable downlink signal.
Uplink:
Maximum path loss at 146 MHz = 145.28 dB
Maximum path loss at 435 MHz = 154.73 dB
Maximum path loss at 1270 MHz = 164.06 dB
Assume spacecraft antenna gain of 0 dBi, 10 watts transmitter power,
and the following net antenna gains for the ground station:
146 MHz = 6 dBi
435 MHz = 9 dBi
1270 MHz = 15 dBi
we obtain at the satellite at maximum range received signals as follows:
146 MHz = -99.28 dBm
435 MHz = -105.73 dBm
1270 MHz = -109.06 dBm
So 146 MHz, 435 MHz or 1270 MHz will provide a workable uplink signal.
Doppler shift:
146 MHz = 3.45 KHz
435 MHz = 10.3 KHz
1270 MHz = 30.1 KHz
So 146 MHz or 435 MHz will provide a workable uplink signal.
1270 MHz will work but will require special doppler compensation.
Last updated 22/07/2002