Experimental Plan for Testing the UNM Metamaterial Slow Wave Structure for High Power Microwave Generation

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Transcription:

Experimental Plan for Testing the UNM Metamaterial Slow Wave Structure for High Power Microwave Generation Kevin Shipman University of New Mexico Albuquerque, NM MURI Teleseminar August 5, 2016 1

Outline 1. Metamaterial (MTM) structure design and simulation 2. Experimental setup 3. Diagnostics 4. Timeline for Experiment 5. Acknowledgements 2

UNM MTM SWS Alternating split-ring resonators 1 Period Ring Inner Radius = 14 mm Ring Outer Radius = 19 mm Tab Inner Radius = 19 mm Tab Outer Radius = 24 mm Ring Gap = 5mm Tube Inner Radius = 24 mm Total # of Ring = 14 Tab 3

Simulation Setup 3-dimensional fully electromagnetic and fully relativistic particle-in-cell (PIC) code MAGIC was used to simulate and optimize the MTM SWS Input Port Cathode MTM SWS Coaxial RF Extraction Antenna Output Port 4

Simulation Results Diode Voltage Input Power Figure 1 400 kv Diode Current Figure 3 1.8 GW Output Power 4.5 ka 160 MW ~ 9% Figure 2 Figure 4 5

Early Simulation Results Cont. RF Signal Measured at Output Port TFA of RF Signal Figure 1 FFT of RF Signal 1.45 GHz (L-Band) Figure 3 RF Output Mode Figure 2 2.472 ns 12.097 ns Figure 4 12.451 ns 6

Experimental Setup SINUS-6 Electron Beam Accelerator 1. Prime Power 2. Tesla Transformer (700 kv, 6kA) 3. Nitrogen Switch (200 psi) 4. Impedance Transformer (20-100 ) 5. Magnetically Insulated Oil-Vacuum Interface 6. Load UNM MTM SWS Drive Voltage : 400 kv Load Current : 4.5 ka B-field : 1.6 T 7

Voltage and Current Diode Diagnostics Oil to Vacuum Interface Rogowski Coil: Current Diagnostic Microwave Window 9 Solenoid Magnets: 1.6 Tesla Antenna Cathode Shank Graphite Cathode Capacitive Divider Probe: Voltage Diagnostic MTM SWS 14 Split Rings Beam Collection Tube and RF Coupler 8

Power Diagnostic A calorimeter is used to measure RF power The calorimeter constitutes a cavity constructed from plexi-glass plates that is filled with ethanol The calorimeter is placed opposite the radiating antenna Incident microwave energy causes expansion of ethanol into capillary tube Ethanol moving into the capillary tube provides a voltage change between two parallel filaments 9

Frequency Diagnostic A Waveguide detector will be used to detect the RF frequency Positioned where E-field is at a maximum A waveguide to coax adapter is used to deliver the RF signal to an Oscilloscope Antenna Coax Cable Waveguide Detector 10

Mode Characterization Use a Neon grid to verify RF mode Neon Grid Electric Field incident on board causes excitation in neon bulbs A time integrated image will be taken with an open shutter camera Neon Grid excited by TE 11 Mode 11

Breakdown in MTM SWS The maximum RF voltage measured between two rings and between the ring and the tube is about 250 kv with gap between the rings being 5mm. Because the spacing between the rings is so small there is a concern for breakdown. Figure 1 Voltage Between Rings Voltage Between Ring and Tube To minimize the chances of breakdown the corners and edges will be rounded and the rings are going to be polished. Figure 2 12

Diagnostic to Measure for Electrical Breakdown 16 Ch. Linear Array Multi-anode PMT: H10515B-20 Developed by Hamamatsu Photonics 0.6-ns response time Gain of 120 db s Convert light from breakdown to electrical signal 4 collimating lenses will be used to collect light Housing for PMT PMT Collimating Lens 13

Breakdown Diagnostic Setup Load Collimating Lenses Fiber Optic Patch Cables Fiber Optic Bulk Head Screen Room Antenna Optical Mount Oscilloscope PMT Array 14

Breakdown Diagnostic Setup Cont. We will mask off the center part of the lenses to block any light coming out of the beam collector tube Lenses will collect light from top and bottom of rings where breakdown is more likely to occur. Blue light has been present in previous experiments on the SINUS-6. Filtering out this blue light maybe needed so the PMT doesn t Saturate Masking Lenses Masking Diagram Light Structure Masking Collimating lenses 15

Timeline August 8 th : Receive SWS and antenna from machining August 9 th - 12 th : Preliminary checks on SINUS-6 August 15 th -24 th : Experimental setup August 25 th -31 st : Run Experiments and Results Analysis 16

Acknowledgments Dr. Sarita Prasad- Research Professor ECE Dmitrii A. Andreev Undergraduate Electrical Engineering Dr. Mark Gilmore Associate Professor, Associate Chair ECE Dr. Edl Schamiloglu-Distinguished Professor, Director of COSMIAC 17