TY - JOUR
T1 - A compact, light-weight high data-rate antenna system for remote-sensing orbiters and space exploration
AU - Harder, Jan
AU - Stoll, Enrico
AU - Schiffner, Michael
AU - Pfeiffer, Matthias
AU - Walter, Ulrich
PY - 2009/12
Y1 - 2009/12
N2 - Upcoming space missions utilizing hyperspectral or other high-resolution sensors will generate a vast amount of data in orbit. The average communication duration between a spacecraft in low Earth orbit (LEO) to a dedicated ground station is short and in addition, due to the high amount of data to be transferred at link times, a high-performance communication system on board of the satellite is indispensable. A solution that provides longer acquisition times with the ground station is to employ a high data-rate inter-satellite link to a geostationary relay satellite, which requires a flat, compact, steerable, light-weight yet robust antenna. Such an antenna system (antenna module plus pointing module) was developed for S-Band at the Institute of Astronautics (Technische Universität München), in cooperation with German space companies, research institutes and the German Aerospace Center (DLR). Its successful operation via the geostationary relay satellite Artemis was demonstrated in cooperation with ESA in 2007. This paper describes the evaluation of an antenna system in the Ka-Band, as a successor to be developed in the next two years for high data rates and the various applications of such an antenna system.
AB - Upcoming space missions utilizing hyperspectral or other high-resolution sensors will generate a vast amount of data in orbit. The average communication duration between a spacecraft in low Earth orbit (LEO) to a dedicated ground station is short and in addition, due to the high amount of data to be transferred at link times, a high-performance communication system on board of the satellite is indispensable. A solution that provides longer acquisition times with the ground station is to employ a high data-rate inter-satellite link to a geostationary relay satellite, which requires a flat, compact, steerable, light-weight yet robust antenna. Such an antenna system (antenna module plus pointing module) was developed for S-Band at the Institute of Astronautics (Technische Universität München), in cooperation with German space companies, research institutes and the German Aerospace Center (DLR). Its successful operation via the geostationary relay satellite Artemis was demonstrated in cooperation with ESA in 2007. This paper describes the evaluation of an antenna system in the Ka-Band, as a successor to be developed in the next two years for high data rates and the various applications of such an antenna system.
KW - Inter-satellite link
KW - Ka-Band
KW - Real-time communication
UR - http://www.scopus.com/inward/record.url?scp=70349776234&partnerID=8YFLogxK
U2 - 10.1016/j.actaastro.2009.05.001
DO - 10.1016/j.actaastro.2009.05.001
M3 - Article
AN - SCOPUS:70349776234
SN - 0094-5765
VL - 65
SP - 1738
EP - 1744
JO - Acta Astronautica
JF - Acta Astronautica
IS - 11-12
ER -