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Waveguide Power Combiner Demonstration for Multiple High Power Millimeter Wave TWTAsNASA is presently developing nuclear reactor technologies, under Project Prometheus, which will provide spacecraft with greatly increased levels of sustained onboard power and thereby dramatically enhance the capability for future deep space exploration. The first mission planned for use of this high power technology is the Jupiter Icy Moons Orbiter (JIMO). In addition to electric propulsion and science, there will also be unprecedented onboard power available for deep space communications. A 32 GHz transmitter with 1 kW of RF output power is being considered to enable the required very high data transmission rates. One approach to achieving the 1 kW RF power, now being investigated at NASA GRC, is the possible power combining of a number of 100-1 50 W TWTs now under development. The work presented here is the results of a proof-of-concept demonstration of the power combining Ka-band waveguide circuit design and test procedure using two Ka- band TWTAs (Varian model VZA6902V3 and Logimetrics model A440/KA-1066), both of which were previously employed in data uplink evaluation terminals at 29.36 GHz for the NASA Advanced Communications Technology Satellite (ACTS) program. The characterization of the individual TWTAs and power combining demonstration were done over a 500 MHz bandwidth from 29.1 to 29.6 GHz to simulate the Deep Space Network (DSN) bandwidth of 3 1.8 to 32.3 GHz. Figures 1-3 show some of the power transfer and gain measurements of the TWTAs using a swept signal generator (Agilent 83640b) for the RF input. The input and output powers were corrected for circuit insertion losses due to the waveguide components. The RF saturated powers of both ACTS TWTAs were on the order of 120 W, which is comparable to the expected output powers of the 32 GHz TWTs. Additional results for the individual TWTAs will be presented (AM/AM, AM/PM conversion and gain compression), some of which were obtained from swept frequency and power measurements using a vector network analyzer. The results for the power combining demonstration as well as a more detailed description of the power combining test circuit and test procedure will also be presented.
Document ID
20050203960
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Wintucky, Edwin G.
(NASA Glenn Research Center Cleveland, OH, United States)
Simons, Rainee N.
(NASA Glenn Research Center Cleveland, OH, United States)
Lesny, Gary G.
(Alphaport, Inc. Cleveland, OH, United States)
Glass, Jeffrey L.
(Lockheed Martin Corp. Cleveland, OH, United States)
Date Acquired
September 8, 2013
Publication Date
January 1, 2004
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
Paper PI.2
Report Number: Paper PI.2
Meeting Information
Meeting: Fifth IEEE International Vacuum Electronics Conference
Location: Monterey, CA
Country: United States
Start Date: April 27, 2004
End Date: April 29, 2004
Funding Number(s)
WBS: WBS 22-982-10-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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