• DocumentCode
    2061621
  • Title

    SMAP Observatory configuration, from concept to preliminary design

  • Author

    Eremenko, Alexander ; Kastner, Jason ; Hoffman, Pamela

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol. / NASA, Pasadena, CA, USA
  • fYear
    2010
  • fDate
    6-13 March 2010
  • Firstpage
    1
  • Lastpage
    11
  • Abstract
    SMAP (Soil Moisture Active and Passive) is a scientific mission to provide global mapping of Earth soil moisture and freeze/thaw state. In order to accomplish this mission the Observatory accommodates two primary Instruments L-band (1.26 GHz) Radar and L-band (1.4 GHz) Radiometer. Both Instruments use a shared 14.6 RPM spinning Antenna System with 6 m diameter deployable Reflector. The key challenges for the Observatory configuration are accommodation of the primary Instruments (Radar and Radiometer), and the supporting subsystems, all the while meeting all operations, pointing, environment requirements, and launch vehicle accommodation. This paper will describe the evolution of the SMAP Observatory configuration and major trade-offs from conceptual to preliminary design.
  • Keywords
    geophysical equipment; radiometers; radiometry; spaceborne radar; 14.6 RPM spinning Antenna System; 6 m diameter deployable Reflector; Earth soil moisture; L-band Radar; L-band Radiometer; SMAP Observatory configuration; Soil Moisture Active and Passive; freeze state; frequency 1.26 GHz; frequency 1.4 GHz; thaw state; Earth; Instruments; L-band; Observatories; Radar antennas; Radiometry; Reflector antennas; SMAP mission; Soil moisture; Spinning;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2010 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-3887-7
  • Electronic_ISBN
    1095-323X
  • Type

    conf

  • DOI
    10.1109/AERO.2010.5446761
  • Filename
    5446761