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X-Band, 17-Watt Solid-State Power AmplifierAn advanced solid-state power amplifier that can generate an output power of as much as 17 W at a design operating frequency of 8.4 GHz has been designed and constructed as a smaller, lighter, less expensive alternative to traveling-wave-tube X-band amplifiers and to prior solid-state X-band power amplifiers of equivalent output power. This amplifier comprises a monolithic microwave integrated circuit (MMIC) amplifier module and a power-converter module integrated into a compact package (see Figure 1). The amplifier module contains an input variable-gain amplifier (VGA), an intermediate driver stage, a final power stage, and input and output power monitors (see Figure 2). The VGA and the driver amplifier are 0.5-m GaAs-based metal semiconductor field-effect transistors (MESFETs). The final power stage contains four parallel high-efficiency, GaAs-based pseudomorphic high-electron-mobility transistors (PHEMTs). The gain of the VGA is voltage-variable over a range of 10 to 24 dB. To provide for temperature compensation of the overall amplifier gain, the gain-control voltage is generated by an operational-amplifier circuit that includes a resistor/thermistor temperature-sensing network. The driver amplifier provides a gain of 14 dB to an output power of 27 dBm to drive the four parallel output PHEMTs, each of which is nominally capable of putting out as much as 5 W. The driver output is sent to the input terminals of the four parallel PHEMTs through microstrip power dividers; the outputs of these PHEMTs are combined by microstrip power combiners (which are similar to the microstrip power dividers) to obtain the final output power of 17 W.
Document ID
20110014705
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other - NASA Tech Brief
Authors
Mittskus, Anthony
(California Inst. of Tech. Pasadena, CA, United States)
Stone, Ernest
(California Inst. of Tech. Pasadena, CA, United States)
Boger, William
(General Dynamics Decision Systems Scottsdale, AZ, United States)
Burgess, David
(General Dynamics Decision Systems Scottsdale, AZ, United States)
Honda, Richard
(General Dynamics Decision Systems Scottsdale, AZ, United States)
Nuckolls, Carl
(General Dynamics Decision Systems Scottsdale, AZ, United States)
Date Acquired
August 25, 2013
Publication Date
January 1, 2005
Publication Information
Publication: NASA Tech Briefs, January 2005
Subject Category
Man/System Technology And Life Support
Report/Patent Number
NPO-30663
Distribution Limits
Public
Copyright
Public Use Permitted.
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