Hi Bob, W7LRD

  I need to answere your question as well via AMSAT-BB because my emails sent 
to [email protected] are alwais rejected to me by your provider. 

  From the point of view of Amateur Radio the best I can suggest to you is the 
book  " The Satellite Experimenters Handbook " by Martin Davidoff K2UBC 2nd 
Edition ARRL Order No 3185  ISBN 0-87259-318-5 and also the ARRL " UHF 
MICROWAVE Experimenters's Manual" ARRL Order No 3126 ISBN 0-87259-312-6 

  Those books  are  full of easy calculations and you can follow it using a 
small scientific hand held calculator but very important  every chapter of the 
UHF MICROWAVE Experimenter's Manual is full of "References and Bibliography " 
that you can find and read/study  to go deeply into details on the above matter 
covering circuits and antennas which are described here in hardware but also 
with related easy to follow calculations.

  At the beginning you must go slowly with the above two books but after a few 
months you will improve and the above matter will come very familiar to you 
provided that you implement your knoledge following the recommended References 
and Bibliography.

  In AMSAT-BB I  follow your experimental activity particularly into the S 
band.............congrats !

  Best 73" de

  i8CVS Domenico 

  ----- Original Message ----- 
  From: Bob- W7LRD 
  To: i8cvs 
  Sent: Wednesday, October 28, 2009 3:23 AM
  Subject: Re: [amsat-bb] Re: requesting help on a RF link solution (imaginary 
ka-bandlink!)


  Hello Domenico

  I enjoy your posts, even though many are "out of my pay grade".  Would you 
aim me towards a good tutorial place you may know of where I could learn some 
of the basics.  I would like to gain a better understanding of this concept.

  Thanks & 73

  Bob W7LRD



  ----- Original Message -----
  From: "i8cvs" <[email protected]>
  To: "Samudra Haque" <[email protected]>, "Amsat-bb" <[email protected]>
  Sent: Tuesday, October 27, 2009 5:44:14 PM GMT -08:00 US/Canada Pacific
  Subject: [amsat-bb] Re: requesting help on a RF link solution (imaginary 
ka-bandlink!)

  ----- Original Message -----
  From: "Samudra Haque" <[email protected]>
  To: "Amsat-bb" <[email protected]>
  Sent: Tuesday, October 27, 2009 11:03 AM
  Subject: [amsat-bb] requesting help on a RF link solution (imaginary
  ka-bandlink!)

  > Hi, amsat-bb
  >
  > CQ any satellite link budget expert !
  >
  > I'm trying to do a calculation on my own based upon published specs
  > for the NASA MRO Ka-band experiment, but am getting some unexpected
  > results for a Ka-band simplex link with Temp=3000K (hypothetical),
  > operating with a Signal to Noise ratio (unitless) figure of 1.171
  > (representing 4.5 dB eb/no with a data rate of 1 Gbps and a bandwidth
  > of 2.4x10^9 Hz)
  >
  > Question : is 1 gbps not 1x10^9 bps ?
  >
  > Question : if both antennas are 3m parabolic (both are the same type)
  > with 56.4 dBi boresight gain, what would you think the furthest
  > distance the link can perform with SNR of 1.171. I have actually used
  > a padding of 3 dB Eb/No in my link budget, so am not worried about any
  > further signal loss at first (ok, I should be ..) For the exercise, I
  > am choosing a 10 Watt estimated output on an arbitrary basis.
  >
  > So:
  >
  > P_t = 10W
  >
  > G_t = 56.4 dBi = G_r , can we assume the same gain for TX and RX on a
  > parabolic dish ?
  >
  > T = 3000K at receiver
  >
  > SNR = 1.171 required
  >
  > f=32.2 GHz
  >
  > B = 2.4E9 Hz, (bpsk, ldpc code 0.5)
  >
  > DR = 1E9 bps
  >
  > So, I am puzzled why this link budget says the range with these
  > parameters is equal to 4.644 x 10^9 Km -- that seems to be a long
  > distance ! What am I not able to conceptualize.
  >
   > BTW, I know if I send this out, the answer will come to me soon
  > thereafter, but for education, I would like to know where the problem
  > in my understanding lies !
  >
  > Samudra N3RDX

  Hi Samudra, N3RDX

  If I well understand your question is to know what is the maximum
  free space distance at which you can get a S/N ratio of 4.5 dB using
  two identical  transmitting and receiving systems having the following
  characteristics:

  1) Antenna gain for TX and RX = 56.4 dBi at 32.2 GHz

  2) Frequency = 32.2 GHz

  3) Overall receiving system noise temperature: T = 3000 kelvin

  4) Bandwidth of receiving system = 2.4 x 10^9 Hz

  5) TX power 10 W

  6) Required Signal to Noise ratio S/N at the unknown distance = 4.5 dB

  With the above data we first calculate the receiver noise floor Pn = KTB
  where:

  K = Boltzmann constant = 1.38 x 10^ -23 (Joule/kelvin)
  T = Overall System Noise Temperature = 3000 kelvin
  B = Bandwidth of receiving system = 2.4 x 10^9 Hz 

  Working out the numbers we get the following RX noise floor 

  Pn = (1.38 x 10^ -23) x (3000) x (2.4 x 10^9) = 1 x 10^-10 watt

  and 10 x  [ log   (1 x 10^-10)] = - 100 dBW or  - 70 dBm
                         10

                                         Link budged calculation

  TX power = 10 W =..................+ 40 dBm
  TX antenna gain ........................+ 56.4 dBi
                                                       ------------
  Transmitted EIRP......................+ 96.4 dBm

  Free space attenuation for
  61.000 km at 32.2 GHz............- 218.3 dB
                                                       ------------
  Received power over isotropic
  ant. at 61.000 km distance........- 121.9 dBm

  RX  antenna gain.......................+56.4 dB
                                                       -------------
  Received power at RX input... - 65.5  dBm
  Receiver noise floor.................- 70.0  dBm
                                                      --------------
  Received S/N Ratio................. + 4.5 dB

  Conclusion:

  Using two boresight identical parabolic dishes having each a gain of
  56.4 dBi at 32.2 GHz one transmitting with 10 watt and the other one
  receiving with a receiving system having a noise temperature of 3000 kelvin
  into a bandwidth = 2.4 x 10^9 Hz the free space distance  at which the
  signal is received with a  S/N ratio  = + 4.5 dB  is only 61.000 km so that
  your hypothetical system is not suitable for the NASA MRO Ka-band
  experiment because the distance Earth to Mars is about 1 AU i.e.
  1 Astronomical Unit  corresponding to 149 Million/ km 

  73" de

  i8CVS Domenico






  _______________________________________________
  Sent via [email protected]. 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


_______________________________________________
Sent via [email protected]. 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

Reply via email to