• 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