Information Capacity Improvement for Deep Space Communication Radio Systems Using Companion Relay Satellites

The paper considers methods and mathematical models for calculation of the information capacity of radio systems for deep space communication in the modes of point-to-point transmission, as well as in the modes of relay by “transparent” and regenerative space transponders. The information capacity is studied depending on the distance of the transponder from the mission-oriented spacecraft by the example of the radio system of scientific data transmission from Mars to Earth in the Ka band. The principal possibility of obtaining a gain in the information capacity of deep-space communication radio systems due to the use of space transponders is shown. The requirements for the main parameters of transponder and its distance from the mission-oriented spacecraft are presented. Estimates for the regions of the relay satellite location providing the maximum increase in the information capacity are obtained for various distances between the mission-oriented spacecraft and the receiver.

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Publication Details

Journal
Russian Aeronautics
Published
2024-12-01
DOI
https://doi.org/10.3103/s1068799824040238
Citations
1
Primary Topic
Satellite Communication Systems
Type
article
Field-Weighted Citation Impact
1.30
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article

Information Capacity Improvement for Deep Space Communication Radio Systems Using Companion Relay Satellites

Н. А. Важенин, Alexander Volkovskii, А. П. Плохих, D. D. Boriskin
1 citations
Russian Aeronautics
Satellite Communication Systems
1.30
article

Information Capacity Improvement for Deep Space Communication Radio Systems Using Companion Relay Satellites

Н. А. Важенин, Alexander Volkovskii, А. П. Плохих, D. D. Boriskin
article en
1 citations

Abstract

The paper considers methods and mathematical models for calculation of the information capacity of radio systems for deep space communication in the modes of point-to-point transmission, as well as in the modes of relay by “transparent” and regenerative space transponders. The information capacity is studied depending on the distance of the transponder from the mission-oriented spacecraft by the example of the radio system of scientific data transmission from Mars to Earth in the Ka band. The principal possibility of obtaining a gain in the information capacity of deep-space communication radio systems due to the use of space transponders is shown. The requirements for the main parameters of transponder and its distance from the mission-oriented spacecraft are presented. Estimates for the regions of the relay satellite location providing the maximum increase in the information capacity are obtained for various distances between the mission-oriented spacecraft and the receiver.

Russian AeronauticsVol. 67(4)
Moscow Aviation Institute (RU)
Affordable and clean energy
Openalex Percentile: Top 10%
Satellite Communication Systems
1.30
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