TY - GEN
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 - 2008
Y1 - 2008
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 hence 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 Universitat Munchen), 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 hence 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 Universitat Munchen), 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.
UR - http://www.scopus.com/inward/record.url?scp=77950511013&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:77950511013
SN - 9781615671601
T3 - International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008
SP - 3170
EP - 3176
BT - International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008
T2 - 59th International Astronautical Congress 2008, IAC 2008
Y2 - 29 September 2008 through 3 October 2008
ER -