• DocumentCode
    1940025
  • Title

    The AstroMesh deployable reflector

  • Author

    Thomson, M.W.

  • Author_Institution
    TRW Astro Aerosp., Carpinteria, CA, USA
  • Volume
    3
  • fYear
    1999
  • fDate
    11-16 July 1999
  • Firstpage
    1516
  • Abstract
    The AstroMesh is a mesh reflector for large aperture space antenna systems. It embodies a new concept for deployable space structures: a pair of ring-stiffened, geodesic truss domes, in which the ring is a truss deployed by a single cable. Compared to other mesh reflectors, the AstroMesh achieves uncharacteristically low levels of total mass, stowed volume, surface distortion, cost, and program schedule duration. Several large AstroMesh reflectors are being produced for a series of US built commercial geosynchronous mobile communications spacecraft; first flight is planned for early 2000. The AstroMesh mounted on the Euro-African Satellite Telecommunications (EAST) system, an example of a large aperture mobile communications satellite conceived by Matra Marconi Space, is depicted. Two large models have been qualified for space flight with as-manufactured shape errors of less than D(6/spl times/10/sup -5/) RMS, and repeatability errors below D(5/spl times/10/sup -5/) RMS (where D is the aperture diameter). With current materials and manufacturing techniques, the AstroMesh design can achieve a surface accuracy from all error sources, including in-orbit environments, of D(2.5/spl times/10/sup -5/) RMS. Large margins on a very demanding passive intermodulation (PIM) specification have been achieved consistently.
  • Keywords
    intermodulation; mobile satellite communication; reflector antennas; AstroMesh deployable reflector; EAST system; Euro-African Satellite Telecommunications system; Matra Marconi Space; USA; aperture diameter; as-manufactured shape errors; deployable space structures; geodesic truss domes; geosynchronous mobile communications spacecraft; large aperture space antenna systems; low cost antenna; low mass; low stowed volume; low surface distortion; mesh reflector; mobile communications satellite; passive intermodulation specification; repeatability errors; ring-stiffened domes; space flight; Aerospace materials; Aperture antennas; Artificial satellites; Costs; Job shop scheduling; Manufacturing; Mobile communication; Reflector antennas; Shape; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Antennas and Propagation Society International Symposium, 1999. IEEE
  • Conference_Location
    Orlando, FL, USA
  • Print_ISBN
    0-7803-5639-x
  • Type

    conf

  • DOI
    10.1109/APS.1999.838231
  • Filename
    838231