Development and design of RF components of telemetry system for use on scientific sounding rocket are described; high velocity (Mach 7) of vehicle requires antenna system of low drag and capable of withstanding high temperatures; solid state transmitter, with output approaching one part in 215-260 mc range, uses simple circuits and few parts; method of cross monitoring transmitter and antenna performance of independent RF systems.
Radio frequency telemetry components for Black Brant III rocket
Can Aeronautics Space J
Canadian Aeronautics and Space Journal ; 8 , n 9
1962
9 pages
Article (Journal)
English
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