Syncom engineering report, Volume 1
Syncom Projects Office, United States. National Aeronautics and Space Administration, Goddard Space Flight Center
National Aeronautics and Space Administration, 1966 - Science - 160 pages
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SYNCOM RANGE AND RANGE RATE SYSTEM
12 other sections not shown
accuracy amplifier analysis ANTENNA ELECTRONICS antenna gain apogee motor approximately axial jet bandwidth baseband beacon Camp Roberts carrier levels channel circuits communication experiment Culver City curves degrees delay Doppler drift rate echo suppressor eclipse effects elevation angles error ground station hydrogen peroxide indicated input Lakehurst launch listener panel maneuver measured Minitrack mode modulation N/N db nitrogen noise temperature operation oscillator output parameters percent performance period phase phase detector precession predicted pressure pulse punched range and range range tone recorded reorientation S+N/N satellite seconds shown in Figure signal-plus-noise to noise SOLAR PANEL solar sensor spacecraft specific impulse spin rate spin speed subcarrier subsystem sun angle SUN SENSOR synchronous Syncom Table telemetered telemetry telemetry and command telemetry data telemetry transmitter teletype thermal tracking transfer orbit transmission transmitted transmitter power transponder traveling-wave tube USNS Kingsport values vcor velocity correction wide-narrow ZULU TIME hours