Implementation of an X-band phased-array subsystem in a deep space mission

Author

Srinivasan, Dipak K. ; Vaughan, Robin M. ; Wallis, Robert E. ; Mirantes, M. Annette ; Hill, T. Adrian ; Cheng, Sheng ; Bruzzi, Jonathan R. ; Fielhauer, Karl B.

Author_Institution

Appl. Phys. Lab., Johns Hopkins Univ., Laurel, MD

fYear

2005

fDate

5-12 March 2005

Firstpage

1541

Lastpage

1551

Abstract

The MESSENGER spacecraft, the first mission to the planet Mercury since 1975, will achieve Mercury orbit in 2011. The spacecraft uses two opposite-facing mission-enabling X-band (8.4 GHz) phased-array antennas to achieve high-rate downlink communications. The spacecraft orientation is constrained such that a preferred direction faces the Sun; rotation about the Sun-line is allowable. The main beam of each antenna is steerable in one dimension. These two degrees of freedom allow the main beam of the phased array to be pointed in any direction about the spacecraft. A novel system-level design requires many different subsystems of the spacecraft to interact together to achieve accurate beam-pointing, and thus, high-rate downlink data from Mercury to Earth

Keywords

Earth; Mercury (planet); Sun; microwave antenna arrays; space research; space vehicle antennas; space vehicles; 8.4 GHz; Earth; MESSENGER spacecraft; Mercury; Sun; X-band phased-array antenna; beam-pointing; deep space mission; downlink communications; system-level design; Downlink; Earth; Mercury (planets); Phased arrays; Planetary orbits; Planets; Space missions; Space vehicles; Sun; System-level design;

fLanguage

English

Publisher

ieee

Conference_Titel

Aerospace Conference, 2005 IEEE

Conference_Location

Big Sky, MT

Print_ISBN

0-7803-8870-4

Type

conf

DOI

10.1109/AERO.2005.1559445

Filename

1559445