Experiment- time synchronization of remote stations using syncom satellite
Synchronization and time maintenance between syncom satellite and syncom stations
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Synchronization and time maintenance between syncom satellite and syncom stations
Launching of syncom satellite to determine if control system and communications equipment can be used for advanced sychronous orbit satellites
Syncom c satellite and thrust augmented delta /tad/ launch vehicle
Triaxiality of earth from observations on drift of syncom ii satellite - longitudinal dependence of earth gravitational field
Test requirement plan and general testing procedures for prototype and flight models of Syncom communications satellite
Drift theory for 24 hour inclined satellite in longitude dependent earth gravity field - actual drift of Syncom II
Performance characteristics of frequency translation transponder units for advanced Syncom satellite, and data on multiple access transponder units
Television tests with Syncom II synchronous communications satellite - ground terminals, spacecraft characteristics, and simulated transmission tests
The crew (Commander Frederick H. Hauck, Pilot David M. Walker, Mission Specialists Anna L. Fisher, Dale A. Gardner, and Joseph P. Allen) prepares for the 14th shuttle mission. The Canadian communications satellite TELESAT-H (ANIK) is attached to Payload Assist Module-D (PAM-D) and deployed into geosynchronous orbit on flight day two. Defense communications satellite SYNCOM IV-I is deployed on day three. Allan and Gardner retrieve two malfunctioning satellites (PALAPA-B2 and WESTAR-VI). Fisher operates the remote manipulator system, grappling satellites and depositing them in the payload door.
Synchronous communication satellite - second syncom satellite launching
The objectives of Space Shuttle Mission STS-32 are described along with major flight activities, prelaunch and launch operations, trajectory sequence of events, and landing and post-landing operations. The primary objectives of STS-32 are the deployment of a Navy synchronous communications satellite (Syncom 4) and the retrieval of the Long Duration Exposure Facility (LDEF) launched from the Challenger in April 1984. Secondary STS-32 payloads include a protein crystal growth experiment, the Fluids Experiment Apparatus (FEA) for the investigation of microgravity materials processing, the Mesoscale Lighting Experiment, the Latitude-Longitude Locator Experiment, the Americal Flight Echocardiograph, and an experiment to investigate neurospora circadian rhythms in a microgravity environment.
Polarimeter for determining ionospheric electron content by measuring Faraday rotation of polarized VHF transmission from Syncom satellites
Over 11 hours of three-axis microgravity accelerometer data were successfully measured in the payload bay of Space Shuttle Columbia as part of the Microgravity Disturbances Experiment on STS-32. These data were measured using the High Resolution Accelerometer Package and the Aerodynamic Coefficient Identification Package which were mounted on the Orbiter keel in the aft payload bay. Data were recorded during specific mission events such as Orbiter quiescent periods, crew exercise on the treadmill, and numerous Orbiter engine burns. Orbiter background levels were measured in the 10(exp -5) G range, treadmill operations in the 10(exp -3) G range, and the Orbiter engine burns in the 10(exp -2) G range. Induced acceleration levels resulting from the SYNCOM satellite deploy were in the 10 (exp -2) G range, and operations during the pre-entry Flight Control System checkout were in the 10(exp -2) to 10(exp -1) G range.
Commander Henry W. Hartsfield, STS 41-D mission by listing the following firsts: (a) first Discovery flight; (b) first flight for a commercial payload specialist; (c) first SYNCOM satellite deployed from an orbiter; and (d.) first to deploy 3 satellites. This was also the heaviest stack at lift-off and the heaviest payload. The footage concludes with a film of the mission highlights.
Major communications satellite systems and evaluation of problems encountered in their establishment
Orbital placement and control of Syncom-II SATELLITE
Electronic parts and component reliability for syncom i satellite
Earth equatorial ellipticity from Syncom II SATELLITE longitude drift