DocumentCode
2100685
Title
The New Horizons high gain antenna: reflector design for a spin-stabilized bus at cryogenic temperatures
Author
Schulze, Ron C. ; Hill, Stuart
Author_Institution
Appl. Phys. Lab., Johns Hopkins Univ., Laurel, MD, USA
Volume
2
fYear
2004
fDate
6-13 March 2004
Firstpage
966
Abstract
The New Horizons antenna system is subjected to cryogenic temperatures during the Pluto and KBO encounters. The RF performance of the high gain antenna (HGA) during and after these encounters is critical for the science and communications mission requirements. In order to satisfy these requirements, the angular alignment of the HGA bore-site and spacecraft spin axis must be maintained within 0.2°. The mechanical design and RF performance of the NH HGA performance at cryogenic operational temperatures and gradients across the reflector surface are described. The RF calculations are performed using Ohio State University Satellite Antenna Consortium Software. Mechanical finite element analysis is used to predict surface distortion resulting from gradients across the surface.
Keywords
Pluto; cryogenics; finite element analysis; reflector antennas; space communication links; space vehicles; KBO encounters; Ohio State University Satellite Antenna Consortium Software; Pluto encounter; RF performance; angular alignment; backscatter method; cryogenic operational temperatures; mechanical design; mechanical finite element analysis; new horizons high gain antenna system; reflector design; spacecraft spin axis; spin stabilized bus; surface distortion prediction; surface shape measurement; Cryogenics; Kuiper belt; Performance gain; Pluto; Radio frequency; Reflector antennas; Satellite antennas; Software performance; Space vehicles; Temperature;
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.2004.1367697
Filename
1367697
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