Study of short term phase stability Interim report, 16 Mar. 1964 - 16 Mar. 1965
Parametric amplifiers and tunnel diodes as L-band and S-band down-converters - frequency division multiplexing
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Parametric amplifiers and tunnel diodes as L-band and S-band down-converters - frequency division multiplexing
Tuning range extension of klystrons used for pumping S-band traveling wave masers
High power testing of S-band Cassegrain monopulse cone antenna
Although the design of the Apollo network followed closely behind the Manned Space Flight Network (MSFN) modification for the Gemini program, many site modifications were necessary to provide Apollo support due to the greater scope of the Apollo program. The Apollo program requires instrumentation for support of the S-I, S-11, S IV-B/IU, Command Service Module (CSM) and Lunar Excursion Module (LEM) stages. Command Service Module (CSM) and Lunar Excursion Module (LEM) stages. Support must also be provided at both orbital and lunar distances. Increased data processing capability is required for processing and displaying significantly larger amounts of information. The ground network requires the capability of processing both Pulse Code Modulation (PCM) telemetry and command data for the CSM, LEM, and S IV-B/IU. In various stages of the Apollo program, both tone (on UHF) and digital [on Unified S-Band (USB) and UHF] command capabilities are required. Also at various stages both USB and VHF telemetry links are required.
Orbital tracking program for analysis of data from C-band and S-band radar
Gas ionization and plasma heating by high power microwaves using X-band and S-band frequency magnetrons
Techniques for improving Apollo spacecraft acquisition using S-band equipment
Mean time between failure and confidence limits for unified S-band system of Manned Space Flight Network based on reliability and performance data from unmanned Apollo flights
Transistor circuit driving S-band diode digital shifters for phased array antenna
Tabulated coherent S-band Doppler data from Pioneer 6 and 7 radio tracking, improving astronomical constants and ephemerides for earth- moon system
Tabulated coherent S-band Doppler data from Pioneer 6 and 7 radio tracking, improving astronomical constants and ephemerides for earth- moon system
Active ranging technique devised for VHF or S-band radar systems divides target Doppler frequency by counter-generated number that is proportional to transmitting frequency, thus producing target velocity data in terms of speed and distance relative to target transponder.
Postflight analyses of Apollo 6 radar tracking for unified S-band orbit determination
Correlating residual patterns in earth orbit unified S-band data with errors in station location or time tagging for postflight analysis
Transient Faraday rotation of S-band telemetry carrier observed during Pioneer 6 occultation by solar corona, correlating with decametric solar radio bursts
Quasi-optical waveguide component /attenuator/ in S-band measured for performance noting diffraction as limiting factor
Parametric amplifier for tracking antenna - Apollo project
Apollo precision frequency source and time standard