DocumentCode :
3555148
Title :
Space tube with high efficiency cooling design approach
Author :
Scherba, M.K.
Author_Institution :
Hughes Aircraft Company, Torrance, California
Volume :
26
fYear :
1980
fDate :
1980
Firstpage :
164
Lastpage :
167
Abstract :
Heat pipes, utilized in a high power space type traveling-wave tube, provide an efficient means of dispersing heat from areas of high concentration. Heat, generated in the region of the collector and output Circuit, is dispersed throughout the entire tube baseplate area by both longitudinal and transverse heat pipes contained in the baseplate. The results are lowered individual component temperatures and reduced thermal densities throughout the baseplate. The objective of this effort was to extend the power level of helix space tubes by combining a high efficiency cooling design approach with high efficiency electrical design techniques previously demonstrated on lower power space devices. These techniques include velocity tapering of the helix circuit, multi-stage depressed electron collection, low dielectric and conductive shield loading, and integral barrel focusing. A novel technique for transferring barrel heat to the baseplate is introduced. The tube delivers 300 watts of continuous wave RF output power at lower E-band frequencies. Saturated gain levels of 40 dB are obtained at an overall efficiency of 52%. The tube has been designed for conservative cathode loading and exhibits low operating temperature.
Keywords :
Circuits; Dielectrics; Distributed power generation; Electrons; Heat transfer; Space cooling; Space exploration; Space heating; Temperature; Trigeneration;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electron Devices Meeting, 1980 International
Type :
conf
DOI :
10.1109/IEDM.1980.189782
Filename :
1481225
Link To Document :
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