DocumentCode
2106042
Title
The RF telecommunications system for the New Horizons mission to Pluto
Author
DeBoy, Christopher C. ; Haskins, Christopher B. ; Brown, Thomas A. ; Schulze, Ronald C. ; Bernacik, Mark A. ; Jensen, I. Robert ; Millard, Wesley ; Duven, Dennis ; Hill, Stuart
Author_Institution
Appl. Phys. Lab., Johns Hopkins Univ., Laurel, MD, USA
Volume
3
fYear
2004
fDate
6-13 March 2004
Abstract
This work describes the design and development of the RF telecommunications system for the New Horizons mission, NASA´s planned mission to Pluto. The system includes an advanced, low-power digital receiver, and a card-based transceiver implemented within an integrated electronics module. An ultrastable oscillator (USO) provides the precision frequency reference necessary for the uplink radio science experiment. The 2.1 meter high gain antenna is the primary communications antenna, with medium gain and low gain antennas used for wider beamwidths during early operations, cruise-phase and sun-pointing mission phases. The paper will discuss the salient aspects of the system design, including design drivers from mission operations, science, and spacecraft considerations. It will also detail individual subsystems1 performance, operational modes (including beacon mode operation), and navigation technology, including the first deep-space flight implementation of regenerative ranging.
Keywords
Pluto; radio receivers; space communication links; space vehicles; ultra wideband communication; NASA; New Horizons mission; Pluto; RF telecommunications system; beacon mode operation; communications antenna; integrated electronics module; low-power digital receiver; navigation technology; operational modes; radio science experiment; spacecraft; subsystems performance; transceiver; ultrastable oscillator; Downlink; Gold; Instruments; Laboratories; Navigation; Physics; Pluto; Radio frequency; Radiometry; Space vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2004. Proceedings. 2004 IEEE
ISSN
1095-323X
Print_ISBN
0-7803-8155-6
Type
conf
DOI
10.1109/AERO.2004.1367922
Filename
1367922
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