A multiple-access satellite relay system for low data rate users
Broad beam Tracking Data Relay Satellite /TDRS/ for manned and automated spacecraft using VHF bands
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Broad beam Tracking Data Relay Satellite /TDRS/ for manned and automated spacecraft using VHF bands
Relay control design for model-tracking system with parameter uncertainties and disturbances using semidefinite Liapunov function
S band communications repeater using retrodirective phased array on synchronous altitude data relay satellite /DRS/ for intersatellite and ground links
Geostationary tracking and data relay satellites /tdrs/, discussing system design and advantages
Relay control systems stability bound determination in nonphase variable form, assuming unknown system parameters
Tracking and data relay satellite system in low altitude synchronous orbit
Tracking and data relay satellite system performance by ATS and Nimbus spacecraft for range and range rate tracking and command and data transmission
Design and telecommunications capabilities of Mark 1 tracking and data relay satellite
Detector provides go/no-go sensing of momentary relay or contact opening during vibration testing. Device compares duration of unwanted openings to calibrated standard and lights indicator if standard is exceeded. Stability and reliability are higher than in any other comparable device.
Multipath operation of low altitude satellite using data relay satellite system
Analysis of low altitude satellite operating in conjunction with data relay satellite system - Phase 2
ATS-F Nimbus E tracking and data relay experiment
Linear repeater design for tracking and data relay satellite system
Time division relay synchronizer with master sync pulse for activating binary counter to produce signal identifying time slot for station
Spiral and helical UHF antennas for home TV reception via satellite broadcast relay system
Relay circuit breaker with magnetic latching to provide conductive and nonconductive paths for current devices
Relay data link and trajectory design integration for Viking orbiter 1975 mission
Jupiter atmospheric probe using relay-link communications geometry between probe and flyby spacecraft for 3.5 hr intervals