Abstracts. International Vacuum Electronics Conference 2000 (Cat. No.00EX392)
DOI: 10.1109/ove:ec.2000.847414
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Advances in space TWT efficiencies

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Cited by 4 publications
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“…The EPC consists of several components including DC‐DC and DC‐Alternating Current (AC) converters, protection circuits, and telecommand‐telemetry circuits . The EPC directly interfaces with the satellite bus primary power and converts the satellite bus voltage to the necessary electrode voltage (kV DC) for the TWT . The EPC can supply thousands of volts of regulated power for stable TWT output power (minimizing the impact of effects such as intermittent power generation and thermal variation experienced during periods of sunlight and eclipse) .…”
Section: Traveling Wave Tube Amplifiersmentioning
confidence: 99%
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“…The EPC consists of several components including DC‐DC and DC‐Alternating Current (AC) converters, protection circuits, and telecommand‐telemetry circuits . The EPC directly interfaces with the satellite bus primary power and converts the satellite bus voltage to the necessary electrode voltage (kV DC) for the TWT . The EPC can supply thousands of volts of regulated power for stable TWT output power (minimizing the impact of effects such as intermittent power generation and thermal variation experienced during periods of sunlight and eclipse) .…”
Section: Traveling Wave Tube Amplifiersmentioning
confidence: 99%
“…Approximately 70% of the total consumed power is converted into RF energy, and the remaining 30% is converted to waste heat. The largest fraction of waste heat is in the collector; therefore, one of the primary focuses for improving amplifier efficiency is to reduce this fraction . Passive thermal control including heat pipes and surfaces of high emissivity is used to dissipate the concentrated heat in the payload .…”
Section: Traveling Wave Tube Amplifiersmentioning
confidence: 99%
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“…It is one of the most critical and expensive components of a satellite. In a typical satellite having 40 TWTs of 100 W RF output power each, the total reduction in launch cost of a satellite reported recently is about US $ 1,000,000 for improving TWT efficiency by 1 % [2]. This figure attract the researchers to work on different parameters to enhance the overall efficiency of the space TWT.…”
mentioning
confidence: 99%