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  • 1
    Publication Date: 2019-06-27
    Description: The transfer function of the retroreflector array carried by the LAGEOS satellite (1976 39A) was computed at three wavelengths: 5230, 6943, and 106000 A. The range correction is given for extrapolating laser range measurements to the center of gravity of the satellite. The reflectivity of the array was calculated for estimating laser-echo signal strengths.
    Keywords: OPTICS
    Type: NASA-CR-157182
    Format: application/pdf
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  • 2
    Publication Date: 2019-06-27
    Description: The transfer function of the retroreflector array carried by the Geos 3 satellite was computed at three wavelength: 5300, 6943, and 10600 A. The range correction is given for extrapolating laser range measurements to the center of gravity of the satellite. The reflectivity of the array was computed for estimating laser-echo signal strengths.
    Keywords: OPTICS
    Type: NASA-CR-145479
    Format: application/pdf
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  • 3
    Publication Date: 2019-06-27
    Description: An optical transfer function was computed for the retroreflector array carried by the Starlette satellite (1975 10A). The range correction is given for extrapolating laser range measurements to the center of mass of the satellite. The gain function and active reflecting area of the array are computed for estimating laser-echo signal strengths.
    Keywords: OPTICS
    Type: NASA-CR-142291
    Format: application/pdf
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  • 4
    Publication Date: 2019-06-27
    Description: An optical transfer function was computed for the retroreflector array carried by the NTS-1 satellite. Range corrections are presented for extrapolating laser range measurements to the center of mass of the satellite. The gain function of the array was computed for use in estimating laser-echo signal strengths.
    Keywords: OPTICS
    Type: NASA-CR-140667
    Format: application/pdf
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  • 5
    Publication Date: 2019-06-27
    Description: Techniques and equations used in calculating the transfer functions to relate the observed return laser pulses to the center of mass of the Lageos satellite retroflector array, and for most of the retroreflector-equipped satellites now in orbit are described. The methods derived include the effects of coherent interference, diffraction, polarization, and dihedral-angle offsets. Particular emphasis is given to deriving expressions for the diffraction pattern and active reflecting area of various cube-corner designs.
    Keywords: OPTICS
    Type: NASA-CR-157932 , SAO-SPECIAL-REPT-382
    Format: application/pdf
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