DocumentCode
3038105
Title
Ka-band feed arrays for spacecraft reflector antennas with limited scan capability-an overview
Author
Jamnejad, V.
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fYear
1992
fDate
2-7 Feb. 1992
Firstpage
57
Lastpage
66
Abstract
The design and breadboard of an active transmitting array at Ka-band frequencies and its application to a reflector antenna system is described. The array is intended as a feed array in a near-field Cassegrain or Gregorian dual-reflector antenna system. It uses tapered slot (Vivaldi) elements in a break architecture. The array has been tested for RF performance. Its performance is acceptable, but there are some areas where improvements in the performance are possible. It was found that particular attention must be paid to the losses at the input to the array elements and in the element itself. Variation of the array phase center in different azimuth planes is another area of concern. The Vivaldi elements have a linear polarization and do not lend themselves easily to a circularly polarized arrangement. For lower losses and circular polarization, microstrip patch arrays in a tile configuration were found to be more advantageous.<>
Keywords
antenna feeders; antenna phased arrays; microstrip antennas; microwave antenna arrays; mobile antennas; reflector antennas; space communication links; space vehicles; Gregorian dual-reflector antenna; Ka-band feed arrays; RF performance; Vivaldi elements; active transmitting array; break architecture; circular polarization; linear polarization; microstrip patch arrays; near-field Cassegrain antenna; spacecraft reflector antennas; tapered slot; tile configuration; Antenna arrays; Antenna feeds; Azimuth; Microstrip antenna arrays; Phased arrays; Polarization; Radio frequency; Reflector antennas; Testing; Transmitting antennas;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Applications Conference, 1992. Digest., 1992 IEEE
Conference_Location
Snowmass, CO, USA
Print_ISBN
0-7803-0225-7
Type
conf
DOI
10.1109/AERO.1992.200375
Filename
200375
Link To Document