DocumentCode :
3201915
Title :
Uplink array concept demonstration with the EPOXI spacecraft
Author :
Vilnrotter, V. ; Lee, D. ; Cornish, T. ; Tsao, P. ; Paal, L. ; Jamnejad, V.
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA
fYear :
2009
fDate :
7-14 March 2009
Firstpage :
1
Lastpage :
8
Abstract :
Uplink array technology is currently being developed for NASA´s deep space network (DSN), to provide greater range and data throughput for future NASA missions, including manned missions to Mars and exploratory missions to the outer planets, the Kuiper belt, and beyond. The DSN uplink arrays employ N microwave antennas transmitting at X-band to produce signals that add coherently at the spacecraft, thereby providing a power gain of N2 over a single antenna. This gain can be traded off directly for N2 higher data rate at a given distance such as Mars, providing for example HD quality video broadcast from earth to a future manned mission, or it can provide a given data-rate for commands and software uploads at a distance N times greater than possible with a single antenna. The uplink arraying concept has been recently demonstrated using the three operational 34-meter antennas of the Apollo complex at goldstone, CA, which transmitted arrayed signals to the EPOXI spacecraft. Both two-element and three-element uplink arrays were configured, and the theoretical array gains of 6 dB and 9.5 dB, respectively, were demonstrated experimentally. This required initial phasing of the array elements, the generation of accurate frequency predicts to maintain phase from each antenna despite relative velocity components due to earth-rotation and spacecraft trajectory, and monitoring of the ground system phase for possible drifts caused by thermal effects over the 16 km fiber-optic signal distribution network. This paper provides a description of the equipment and techniques used to demonstrate the uplink arraying concept in a relevant operational environment. Data collected from the EPOXI spacecraft was analyzed to verify array calibration, array gain, and system stability over the entire 5 hour duration of this experiment.
Keywords :
antenna phased arrays; space communication links; space vehicles; Apollo complex; EPOXI spacecraft; Kuiper belt; Mars; NASA; array element phasing; deep space network; exploratory missions; fiber-optic signal distribution network; gain 6 dB; gain 9.5 dB; microwave antennas; outer planets; software uploads; time 5 hour; uplink array concept demonstration; uplink arraying concept; Antenna arrays; Mars; Microwave antenna arrays; NASA; Phased arrays; Space missions; Space technology; Space vehicles; Throughput; Transmitting antennas;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace conference, 2009 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4244-2621-8
Electronic_ISBN :
978-1-4244-2622-5
Type :
conf
DOI :
10.1109/AERO.2009.4839372
Filename :
4839372
Link To Document :
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