1 Development of a W-Band TE01 Gyrotron Traveling-Wave Amplifier (Gyro-TWT) for Advanced Radar Applications H. H. Song, D. B. McDermott, Y. Hirata, L. R. Barnett*, C. W. Domier, H. L. Hsu, T. H. Chang*, W .C. Tsai*, K. R. Chu*, and N. C. Luhmann, Jr. Department of Applied Science, Univ. of California, Davis *Department of Physics, National Tsing-Hua Univ., Taiwan Motivation Increasing needs for broadband, high power millimeter wave sources for: • High resolution imaging radar • Radar tracking for space debris • Atmospheric sensing (ozone mapping etc.) • Communication systems US Navy 94 GHz High Power WORLOC Radar Why Gyro-TWT (Gyrotron Traveling Wave Tube) ? • Gyro-TWT has a higher power capability ( > 100 kW) than conventional linear TWT • Gyro-TWT has wider bandwidth than other Gyro-devices (Gyroklystron, Gyrotwystron) Univ. of Miami 94GHz Cloud Radar 2 3 UCD W-band TE01 Gyro-TWT Amplifier Objectives Overall system setup for hot test of the W-band TE01 gyro-TWT • Extend the state-of-the-art wide bandwidth, high power millimeter wave amplifier technology by developing a stable W-band gyro-TWT (Goal performance: Pout=110 kW, Gain=45 dB, h=22%, BW3dB=5%) Approach • Gyro-TWT’s offer wide bandwidth • TE01 mode transmits high power • Distributed wall loss configuration stabilizes amplifier Accomplishments • Recent gyro-TWT under hot test with 61.2 kW saturated output power, 40 dB gain, 17.9 % efficiency, 1.5 GHz (1.6%) bandwidth in zero drive stable condition (unoptimized) 4 Dispersion Diagram of TE01 Gyro-TWT 100 kV, a=1.0 w/2p (GHz) 200 • Beam mode dispersion: w = sWc + kzvz Wave mode dispersion: w2 = wc2 +c2kz2 TE02(2) • Absolute instabilities must be stabilized : TE11(1), TE21(1), TE02(2) ,TE01(1) 150 s=2 operating point (grazing intersection) TE01(1) 100 TE21(1) 50 s=1 Potential Gyro-BWO interaction -4000 TE11(1) 0 kz(/m) 4000 Design Approach • Iterate the loop to optimize the gain, power, efficiency, and bandwidth Choose Device parameters Beam voltage, velocity ratio, Mode, guiding center radius etc. Check Large Signal Characteristics Determine stable beam current Simulation using ‘Absolute Instability’ code [1] Simulation using nonlinear code [3] Determine Circuit Length and Loss Value Simulation using ‘Gyro-BWO’ code [2] [1] ‘Absolute Instability’ code is based on K.R.Chu et. al, “Gain and Bandwidth of the Gyro-TWT and CARM Amplifiers”, IEEE Trans. Plasma Sci., vol.16, pp.90-104, 1988) [2] ‘Gyro-BWO’ code is based on C.S.Kou et. al, “High Power Harmonic Gyro-TWT-Linear Theory and Oscillation Study”, IEEE Trans. Plasma Sci., vol.20, pp.155-162, 1992) [3] Nonlinear code is based on (K.R.Chu et. al, “Theory and Experiment of Ultrahigh-Gain Gyrotron Traveling Wave Amplifier”, IEEE Trans. Plasma Sci., vol.27, pp.391-402, 1999) 5 6 Device Parameters Voltage Current a= v^/vz Dvz/ vz Magnetic Field(Bo) Bo/Bg Cutoff Frequency Wall Resistivity Circuit Radius, rw Guiding Center Radius, rc Circuit Length 100 kV 5A 1.0 5% 35.6 kG 0.995 90.97 GHz 70,000 rCu 0.201 cm 0.45 rw 13.6 cm Stable Beam Current • Gyro-TWT exhibits absolute instability near cutoff at sufficiently high beam current • Unloaded TE01 circuit is stable for beam current = 5 A for design value a =1.0 and Bo/Bg= 0.995 • Beam current can be higher for lower a (=v^/vz) and lower Bo/Bg Stability from TE01 Cutoff Oscillation Keep I < Is a = 0.9 Is(A) 1.0 1.1 Design value 1.2 1.3 Bo/Bg Simulation results using ‘Absolute Instability’ code 7 8 Predicted Gyro-TWT Performance • Nonlinear large signal code predicts output power, efficiency and gain For predicted velocity spread Dvz/vz = 5% -Bandwidth Dw/w = 5% - Pout= 110 kW - h = 22% - Large signal gain = 45 dB 9 Application of Loss • Loss has been added to circuit to suppress Gyro-BWO Theory r/rCu = 70,000 is needed • ‘Aquadag’ (a Carbon colloid) has the desired loss of r/rCu 70,000 Measurement versus HFSS simulation Axial view of TE01 Gyro-TWT circuit output loss 12cm 1.6cm • Initial 12 cm is coated. Final 1.6 cm is uncoated to prevent wave damping • 90 dB loss is measured at 93 GHz • Loss lowers the gain but this can be compensated by increasing the circuit length to just below the critical length HFSS-Copper Guide Insertion Loss (dB / 12 cm) input Measurement 0 HFSS-Resistive Guide r/r =70,000) Cu -50 -100 HFSS-Copper Guide with Inner Semiconductor Tube ( Dr=0.05 mm, r/r =70,000) -150 Cu rw=2.01 mm -200 90 92 94 96 98 Frequency (GHz) 100 10 Experimental Design and Setup • Single Anode MIG • High Voltage Modulator • RF Couplers • Interaction Circuit • Vacuum System • Superconducting Magnet System • RF Drive Sources • RF Diagnostics Single Anode MIG Assembled MIG • Designed MIG beam parameters Cathode Beam voltage 100 kV Stalk Beam current 5A Cathode Velocity ratio (v^/ vz) 1.0 Emission Velocity spread 2% Ring Cathode radius 5.1 mm Guiding center radius 0.9 mm Activated MIG Glowing Cathode Emission Ring EGUN simulation of electron trajectory and magnetic field profile 11 RF Couplers • 0 dB input coupler and 10 dB output coupler are employed TE10 TE51 TE01 Coax Coupler Designed with HFSS All Modes are Matched Cross section of the Fabricated Coax Coupler Rectangular Input waveguide (TE10 ) Coaxial Cavity (TE51 ) Interaction Circuit (TE01 ) HFSS cross sectional view of electromagnetic field intensity 12 RF Coupler Characterization 13 • RF couplers are characterized using both scalar and vector network analyzers Input coupler Output coupler Scalar measurement Scalar measurement Vector measurement Vector measurement 14 Interaction Circuit • Interaction region is heavily loaded with ‘Aquadag’, a carbon colloid with r/rcu= 70,000 • Final 1.6 cm of interaction region is unloaded to avoid damping of high power wave Input Coupler Beam Tunnel 30cm ruler Output Coupler Interaction Region (13.6cm) Coated with Aquadag Load Collector Uncoated Axial View of Fabricated TE01 interaction circuit RF Input Driver • W-Band input driver is capable of driving either Hughes Folded Waveguide TWT (94 GHz, 100W, BW=5%) or CPI EIO (93 GHz, 1 kW, BW=5%) SLAC-UC Davis W-Band Modulator Hughes 94 GHz, 100 W Folded Waveguide TWT 15 16 RF Diagnostics • RF diagnostics are setup to monitor the output power w/ and w/o input drive • Various modes are measured simultaniously using waveguide switch, cavity filter, waveguide cutoff sections, and Fabry-Perot interferometer Directional coupler Fabry-Perot interferometer 3 2 Cross guide coupler Variable Circulator attenuator Gyro-TWT OUT IN 2 Ka-Band overmoded waveguide 1 3 Frequency meter High power load Crystal detector scope Input driver 17 Magnet System • Refrigerated Superconducting Magnet Magnetic Field (kG) • Magnetic field profile for 4 coils Superconducting magnet Coil power supply - 50 kG ± 0.1% over 50 cm - 4 compensated independent coils - 6” large bore Axial position (cm) Magnetic Field (kG) Integrated Gyro-TWT System Axial Position of Superconducing Magnet (cm) Gun Vacuum Pump Superconducting Magnet Beam Tunnel MIG RF Input Collector RF Output Main Vacuum Pump 18 Experimental Progress Flowchart 1st version Gyro-TWT 19 - Employed MIG Dvz/vz=5% (predicted) - Small signal gain=34dB, BW=2% - Performance hampered by misaligned MIG (Dvz/vz=10% inferenced by nonlinear code) 2nd version Gyro-TWT - Employed realigned MIG Dvz/vz=2% (predicted) - 59kW output power, 42 dB gain, 26.6% efficiency, and BW=1.3 GHz - Performance limited by spurious oscillations (TE02 and TE01 mode oscillations) 3rd version Gyro-TWT - Employed shortened interaction circuit - 61kW output power, 40 dB gain, 17.9% efficiency, and BW=1.5 GHz - Performance limited by reflections at the output end and gun misalignment 4th - Employed well matched output section and well aligned MIG - Currently under hot test version Gyro-TWT 20 Measured Transfer Characteristics - Gyro-TWT shows good linearity at lower voltages (< 70 kV) • Vb=56 kV, Ib=3.7 A and Bo=34.1 kG 2nd version Gyro-TWT 21 Measured Bandwidth - 1.2 GHz 3 dB bandwidth has been measured • Vb=60 kV, Ib=3.7 A and Bo=34.0 kG 2nd version Gyro-TWT Frequency Identification using Fabry-Perot Interferometer • Fabry-Perot interferometer using two horn antennas, metal mesh, and translational stage employed to identify competing modes horn antenna crystal detector metal mesh micrometer 22 23 Mode Competition Identification 2nd version Gyro-TWT 3rd version Gyro-TWT Shorten circuit length TE02 mode oscillation (170 GHz) TE01 mode drift tube oscillation (85 GHz) TE01 mode cutoff oscillation (91 GHz) Eliminated Reduced drift tube radius Eliminated Shorten circuit length Higher start oscillation current 24 Measured Start Oscillation Current • Start oscillation current for TE01 cutoff oscillation were measured • Oscillation threshold decreases for increasing magnetic field • By shortening circuit length, start oscillation current has been increased 2nd version 3rd version 85 kV 85 kV 60 kV 60 kV Drift Tube Oscillation 25 - In 2nd version, oscillation has been measured at 85 GHz at the drift tube using Fabry-Perot interferometer - TE01 mode at the drift tube has been identified to be the source of oscillation drift tube radius reduced in 3rd version and oscillation eliminated • Cyclotron and cutoff frequency vs. axial position of beam tunnel region cyclotron TE01 cutoff frequency (61 kV) cyclotron TE21 cutoff Frequency (100 kV) TM01 cutoff TE11 cutoff 2nd version Gyro-TWT 26 Mode Competition - 2nd version Gyro-TWT performance limited to lower voltage due to mode competition - Competing mode are identified to be TE02 mode measured at 170 GHz using Fabry-Perot interferometer• Vb=70 kV, Ib=5.3 A, Bo=34.3 kG • Ib=5.4 A, Bo=34.3 kG 2nd version Gyro-TWT 27 Measured Absolute Instability - In 2nd version, oscillations near cutoff frequency (~91 GHz) have been observed at higher voltages than > 70 kV - The cutoff oscillation degrades the amplified signal •Vb=80 kV, Ib=5.1 A, Bo=34.8 kG • Vb=72 kV, Ib=5.3 A, Bo=34.1 kG 2nd version Gyro-TWT 28 Measured Bandwidth - 3rd version gyro-TWT performance limited due to the excessive return loss at the output end (verified by simulation) • Different return loss assumed in simulation • Effect of return loss on bandwidth and comparison with measurement 3rd version Gyro-TWT 29 Improved Output Reflection - Output section reflection has been improved using heavily loaded output load - 10-layer coated output load currently employed in the hot test (4th version gyro-TWT) Summary • UCD 94 GHz TE01 Gyro-TWT has been constructed with predicted capability of 110 kW with Dw/w=5% and h=22%. • Circuit has been heavily loaded to suppress Gyro-BWO with 90 dB loss measured at 93 GHz. • 1st and 2nd version gyro-TWT performance limited by velocity spread and competing modes. • Recent 3rd version gyro-TWT hot tested with 61.2 kW saturated output power, 40 dB gain, 17.9% efficiency, and 1.5 GHz bandwidth (1.6 % BW). • To enhance the bandwidth and the output power, improved output section with reduced reflection and well aligned MIG are employed in the 4th version of gyro-TWT (currently under hot test). 30