Design of an inter-satellite communication and ranging payload for a rendezvous and proximity operations mission

This paper presents the design of an inter-satellite communication and round-trip time-of-flight ranging payload for a rendezvous and proximity operations mission, based around the commercial off-the-shelf transceiver SX1280 by Semtech. The payload is designed to operate in the S-band Space Operations frequency band (from 2.20 to 2.29 GHz), with the ISM band (from 2.4 to 2.5 GHz) available for ground testing.

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Publication Details

Published
2025-01-01
DOI
https://doi.org/10.13164/eeict.2025.84
Primary Topic
Spacecraft Design and Technology
Type
article
Field-Weighted Citation Impact
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article

Design of an inter-satellite communication and ranging payload for a rendezvous and proximity operations mission

Jan Gromeš, Jiří Veverka, Alexander Bekeč
Spacecraft Design and Technology
article

Design of an inter-satellite communication and ranging payload for a rendezvous and proximity operations mission

Jan Gromeš, Jiří Veverka, Alexander Bekeč
article en

Abstract

This paper presents the design of an inter-satellite communication and round-trip time-of-flight ranging payload for a rendezvous and proximity operations mission, based around the commercial off-the-shelf transceiver SX1280 by Semtech. The payload is designed to operate in the S-band Space Operations frequency band (from 2.20 to 2.29 GHz), with the ISM band (from 2.4 to 2.5 GHz) available for ground testing.

Openalex Percentile: Top 72%
Spacecraft Design and Technology
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Design of an inter-satellite communication and ranging payload for a rendezvous and proximity operations mission — Jan Gromeš, Jiří Veverka, et al. · (2025) | TGRS Research Map | TGRS