DocumentCode :
381300
Title :
Maximization of data return at X-band and Ka-band at DSN´s 34-meter beam-waveguide antennas
Author :
Sharnbayati, S.
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
Volume :
3
fYear :
2002
fDate :
2002
Abstract :
In this paper we offer a new approach to evaluating the performance advantage of Ka-band frequency over X-band frequency for the receiving spacecraft downlink from deep space missions. For a given elevation profile for a pass, this approach uses atmospheric noise temperature statistics to select the optimum data rate to maximize the total data return volume over the pass. For illustration purposes, this approach is used to optimize the performance of a link for both X-band and Ka-band at a NASA Deep Space Network (DSN) 34 m Beam Waveguide tracking stations at both Madrid, Spain and Goldstone, California. Our calculations show that using such an approach an optimized Ka-band link offers between 5.9 dB and 7.2 dB more data volume over an optimized X-band link, and between 8.5 dB and 10.3 dB over an X-band link as currently operated by the DSN. It should be noted that the reliability of link designed in such a manner is relatively low and that a link optimized in this manner may not meet the continuity requirements of a mission. Furthermore, this approach takes only the weather effects into consideration. Other factors which may adversely affect the performance of the link are not taken into account under this approach.
Keywords :
atmospheric electromagnetic wave propagation; environmental degradation; noise; optimisation; radio receivers; radiowave propagation; receiving antennas; space communication links; telecommunication network reliability; waveguide antennas; 34 m; DSN; Ka-band data return maximization; NASA Deep Space Network beam waveguide; X-band data return maximization; atmospheric noise temperature statistics; beam-waveguide antennas; data volume; deep space missions; link performance; link reliability; mission continuity requirements; optimized Ka-band link; optimized X-band link; optimum data rate; receiving capabilities; receiving spacecraft downlink; total data return volume; weather effects; Atmospheric waves; Design optimization; Downlink; Frequency; NASA; Space missions; Space stations; Space vehicles; Statistics; Temperature distribution;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference Proceedings, 2002. IEEE
Print_ISBN :
0-7803-7231-X
Type :
conf
DOI :
10.1109/AERO.2002.1035259
Filename :
1035259
Link To Document :
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