[Date Prev][Date Next][Thread Prev][Thread Next] - [Date Index][Thread Index][Author Index]

Re: NASA's American Student Moon Orbiter...

At 05:42 AM 7/4/2008, i8cvs wrote:
>Only considering the 2 meters downlink suppose to put AO40 at 400.000
>km with the antennas pointing at the earth with low squint angle let say
>less than 10 degrees.
>The gain of the AO40 2 meters antennas was 10 dBi and we put your
>10 watt on it.
>Suppose that your 2 meter antenna has a gain of  13 dBi and the overall
>noise figure of your receiving system is NF= 0,7 dB = 51 kelvin so that
>the noise floor into a CW passband of 500 Hz with the antenna looking
>at the moon (200 kelvin) is about -178 dBW
>Suppose that the station in QSO with you has a 70 cm EIRP capability to
>get the full 2 meters 10 watt from the transponder only for you and we
>can calculate it later on.
>2 meters downlink budged calculation:
>Satellite power ................................... + 10 dBW
>Satellite antenna gain.......................... + 10 dBi
>                                                              --------------
>Satellite EIRP..................................... +  20 dBW (100 W EIRP)
>2 m isotr. attenuation  400.000 km..  -188 dB
>                                                              --------------
>power density received on a ground
>isotropic 2 meters antenna..................-168 dBW
>2 m ground station antenna gain.........+ 13 dBi
>                                                              ---------------
>Power density at 2 m RX input...........- 155 dBW
>2 m receiver noise floor......................- 178 dBW
>                                                              ---------------
>Received CW signal S/N.................... + 23 dB
>If we increase the BW to 2500 Hz for a SSB QSO than the noise floor
>of the receiving system increases by log    (2500/500) = 7 dB i.e.
>                                                                  10
>it becames about -171 dB and the SSB signal will be received with a
>S/N ratio = 23-7 = 16 dB wich is a very strong SSB signal.
>Be aware that the above figures are based on the assumption that the
>satellite antennas are pointig toward the earth wich is not the case with
>a moon orbiting satellite.
>In addition we assume that the station in QSO with you has a 70 cm
>EIRP capability in order to get 10 watt from the 2m transponder only
>for you.
>On the other side if a fixed 10 dBi 2 meters antenna is placed over the
>moon and it is oriented toward the earth could easily cover the inclination
>X libration window without any adjustement and only from the point of
>view of the downlink with 10 watt it can be easily used for a transponder
>on the moon.
>If you make again the downlink budged calculation considering that
>the 2 meter transponder will develope only 2.5 watt for  you then you
>will realize that the transponder will accomodate 3 more stations if each
>one is getting 2.5 watt as well.
>In this case your S/N ratio will be still +15.5 dB on CW and +8.5 dB
>in SSB and the same is true for the other 3 users.
>73" de
>i8CVS Domenico

Good example of path link analysis, keeping it simple!

But the trick is limiting input to four stations with a linear 
transponder and they all running an equal uplink.  Reality is this 
doesn't happen so the shared portion of downlink power may and most 
likely will be less with reduced S/N.  My experience with AO-40 was 
that to have a reasonably good SSB contact you needed at least S/N of 
10-dB.  In fact that resulted in a fairly weak signal which was 
difficult to copy.  20-dB S/N made for arm-chair reception.

Not discussed were the 70cm uplink requirements.  I suppose one could 
run high power to achieve that.  My AO-40 experience was running up 
to 60w at a 16.5 dBdc antenna (18.6 dBic).  Most of the time I was 
good with about 5-10w if the satellite was lightly loaded.  But with 
high numbers of stations trying to operate I needed the full EIRP = 
72x60 = 4320w  or in dB:  18.6 + 47.8 = 66.4 dBW

My AO-40 mode-US station consisted of a FT-847+60w linear at the 
antenna (M2-436CP42UG) for uplink.  The 2.4 GHz downlink was a 
33-inch dish with helix feed+MKU-232A2 preamp+Drake converter+FT-847 
(on 123-MHz).

I'm not going to go into those calculations. 

Sent via AMSAT-BB@amsat.org. Opinions expressed are those of the author.
Not an AMSAT-NA member? Join now to support the amateur satellite program!
Subscription settings: http://amsat.org/mailman/listinfo/amsat-bb