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  • COMMUNICATIONS  (12)
  • GEOPHYSICS  (7)
  • Australopithecus africanus  (2)
  • 1
    Publication Date: 2006-01-12
    Description: The Apollo Soyuz Test Project Geodynamics Experiment was performed to assess the feasibility of tracking and recovering high frequency components of the earth gravity field by utilizing a synchronous orbiting tracking station such as Applications Technology Satellite 6. Two prime areas of data collection were selected for this experiment. The first area is the center of the African continent, and the second area is the Indian Ocean depression centered at latitude 5 N and longitude 75 E. Preliminary results show that the detectability objective of the experiment has been achieved in both areas as well as in several additional anomalous areas around the globe. Gravity anomalies of the Karakoram and Himalayan mountain ranges of ocean trenches, and of the Diamantina depth are specific examples.
    Keywords: GEOPHYSICS
    Type: Apollo-Soyuz Test Project; 16 p
    Format: text
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  • 2
    Publication Date: 2011-08-16
    Description: This note deals with the measurement of the total electron content of the ionosphere at the Goddard Space Flight Center, looking towards the geostationary satellite ATS 3 during the solar eclipse of Mar. 7, 1970. Obscuration at this site was nearly total. Faraday rotation was measured with a stationary circularly polarized antenna and a dual-channel phase-lock receiver tuned to 137.350 MHz. By comparing the electrical phase of the two opposite circularly polarized components, a continuous chart recording was made of Faraday rotation vs local time. A depletion of about 25% in electron content was observed from first contact to the time of minimum electron content. The time variations of the electron content during the eclipse are briefly examined in the light of current theories of ionospheric processes.
    Keywords: GEOPHYSICS
    Type: Radio Science; 6; Aug
    Format: text
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  • 3
    Publication Date: 2016-06-07
    Description: Ionospheric bias corrections associated with radio tracking of spacecraft depend on the following measuring techniques for integrated electron content: (1) Faraday rotation measurements from an earth synchronous satellite; (2) ranging measurements at two frequencies; and (3) group and phase velocity measurements obtained from tracking data. The extraction of the integrated electron content directly from tracking data is achieved by comparison of range-rate measurements based on Doppler shift with differentiated range measurements based on tone delay. This method is most desirable because the measured corrections pertain directly to the spacecraft whose orbit is being determined and can be used in near earth as well as deep space tracking data.
    Keywords: COMMUNICATIONS
    Type: Significant Accomplishments in Technol., GSFC, 1970; p 3-9
    Format: application/pdf
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  • 4
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    In:  CASI
    Publication Date: 2019-05-29
    Description: Communication system radio frequency selection for space mission and capsule recovery
    Keywords: COMMUNICATIONS
    Type: NASA-TM-X-55525 , X-507-66-169
    Format: application/pdf
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  • 5
    Publication Date: 2019-05-30
    Description: Tracking errors at S-band and C-band frequencies resulting from diurnal, seasonal, and annual changes in earths atmosphere
    Keywords: COMMUNICATIONS
    Type: NASA-TN-D-3470
    Format: application/pdf
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  • 6
    Publication Date: 2019-06-27
    Description: The Goddard Range and Range Rate System (GRARR) determines the range of a spacecraft by measuring the group delay of a modulated wave and the range rate by measuring the Doppler phase shift of the carrier. An analytical technique is presented for obtaining corrections and equivalent total electron content along the vertical, using VHF GRARR data and a radial model of the ionosphere. The results of computation for a representative pass are given, and estimated accuracy is discussed from a statistical view point. Using VHF GRARR data and a radial model of the ionosphere. The results of computation for a representative pass are given, and estimated accuracy is discussed from a statistical view point. Using GRARR range, range rate, and angle tracking data from Explorer 41, values of total electron content on the order of 10 to the 17th to 10 to the 18th power (electrons/sq m) were obtained. These values agree with estimates of the total electron content from ionospheric profiles using f sub o F sub 2 predict data.
    Keywords: GEOPHYSICS
    Type: NASA-TM-X-65911 , X-551-71-475
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  • 7
    Publication Date: 2019-06-27
    Description: Feasibility of direct relay of Apollo spacecraft data via communication satellite
    Keywords: COMMUNICATIONS
    Type: NASA-TM-X-55627 , X-507-66-310
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  • 8
    Publication Date: 2019-06-27
    Description: Feasibility of direct relay of Apollo spacecraft data via communications satellite
    Keywords: COMMUNICATIONS
    Type: NASA-TN-D-4048
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  • 9
    Publication Date: 2019-06-27
    Description: Influence of atmospheric refraction on minitrack interferometer system and correction procedures for computation accuracy
    Keywords: COMMUNICATIONS
    Type: NASA-TN-D-5966 , G-974
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  • 10
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    In:  CASI
    Publication Date: 2019-06-27
    Description: Tracking performance of Apollo land and ship based C band radar equipment
    Keywords: COMMUNICATIONS
    Type: NASA-TM-X-63049 , X-551-67-503
    Format: application/pdf
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