• DocumentCode
    3047586
  • Title

    Radar altimeter for surface analysis in planetary applications

  • Author

    Picardi, G. ; Seu, R. ; Melacci, P.

  • Author_Institution
    Info-Com Dept., Rome Univ., Italy
  • fYear
    1990
  • fDate
    7-10 May 1990
  • Firstpage
    28
  • Lastpage
    33
  • Abstract
    A new-concept radar altimeter for the ESA-NASA joint mission named Rosetta has been studied. The goal of that mission is to approach and land on a comet nucleus, take a sample of the comet nucleus, and bring it to the Earth. The success of the mission is strongly related to a safe landing on a suitable site. A radar altimeter should perform the main operations during the landing phase giving information not only about attitude and surface roughness but also about the surface composition and the presence and nature of subsurface discontinuities. Surface composition means the type of material giving rise to the observed echo. A comet model, an EM model of the received echo, the radar altimeter operational mode, and optimum system design criteria are discussed in terms of transmitted frequency, pulse repetition frequency and signal bandwidth
  • Keywords
    aerospace instrumentation; cometary nuclei; radioaltimeters; space vehicles; EM model; ESA; NASA; Rosetta mission; attitude; comet nucleus; planetary applications; pulse repetition frequency; radar altimeter; radar echo; signal bandwidth; subsurface discontinuities; surface analysis; surface composition; surface roughness; transmitted frequency; Contracts; Crystalline materials; Dielectric constant; Dielectric materials; Electromagnetic modeling; Frequency; Radar applications; Rough surfaces; Surface roughness; Surface waves;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Radar Conference, 1990., Record of the IEEE 1990 International
  • Conference_Location
    Arlington, VA
  • Type

    conf

  • DOI
    10.1109/RADAR.1990.201132
  • Filename
    201132