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A low-power, high-efficiency Ka-band TWTAA NASA-sponsored program is described for developing a high-efficiency low-power TWTA operating at 32 GHz and meeting the requirements for the Cassini Mission to study Saturn. The required RF output power of the helix TWT is 10 watts, while the dc power from the spacecraft is limited to about 30 watts. The performance level permits the transmission to earth of all mission data. Several novel technologies are incorporated into the TWT to achieve this efficiency including an advanced dynamic velocity taper characterized by a nonlinear reduction in pitch in the output helix section and a multistage depressed collector employing copper electrodes treated for secondary electron-emission suppression. Preliminary program results are encouraging: RF output power of 10.6 watts is obtained at 14-mA beam current and 5.2-kV helix voltage with overall TWT efficiency exceeding 40 percent.
Document ID
19920055539
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Curren, A. N.
(NASA Lewis Research Center Cleveland, OH, United States)
Dayton, J. A., Jr.
(NASA Lewis Research Center Cleveland, OH, United States)
Palmer, R. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Force, D. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Tamashiro, R. N.
(NASA Lewis Research Center Cleveland, OH, United States)
Wilson, J. F.
(NASA Lewis Research Center Cleveland, OH, United States)
Dombro, L.
(Hughes Aircraft Co. Torrance, CA, United States)
Harvey, W. L.
(JPL Pasadena, CA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Subject Category
Electronics And Electrical Engineering
Meeting Information
Meeting: 1991 International Electron Devices Meeting
Location: Washington, DC
Country: United States
Start Date: December 8, 1991
End Date: December 11, 1991
Accession Number
92A38163
Distribution Limits
Public
Copyright
Other

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