Advanced Syncom - Syncom II summary report
Spacecraft systems design, reliability, support equipment, alternate configurations, and radiation instrumentation payload for Syncom II
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Spacecraft systems design, reliability, support equipment, alternate configurations, and radiation instrumentation payload for Syncom II
Synchronization and time maintenance between syncom satellite and syncom stations
Synchronous communication satellite - second syncom satellite launching
Transmission of u.n. general assembly opening by relay i and syncom ii via television and radio
Launching of syncom satellite to determine if control system and communications equipment can be used for advanced sychronous orbit satellites
Range and range rate system and data analysis for syncom i satellite
Triaxiality of earth from observations on drift of syncom ii satellite - longitudinal dependence of earth gravitational field
Electronic parts and component reliability for syncom i satellite
Syncom c satellite and thrust augmented delta /tad/ launch vehicle
Drift theory for 24 hour inclined satellite in longitude dependent earth gravity field - actual drift of Syncom II
Television tests with Syncom II synchronous communications satellite - ground terminals, spacecraft characteristics, and simulated transmission tests
Test requirement plan and general testing procedures for prototype and flight models of Syncom communications satellite
Earth equatorial ellipticity from Syncom II SATELLITE longitude drift
Syncom II launch by three stage thrust-augmented Delta vehicle configuration
Performance characteristics of frequency translation transponder units for advanced Syncom satellite, and data on multiple access transponder units
Use of tracking data from Syncom II satellite to define longitude-dependent gravity field of earth
Syncom-II satellite drift rate in equatorial orbit used to define longitudinal dependence of earth gravitational field
Hypothetical four-body problem applied to estimate effects of moon and sun on Syncom orbit