SPUTTER-WIND HEATING IN IONIZED METAL PVD+ Junqing Lu* and Mark Kushner** *Department of Mechanical and Industrial Engineering **Department of Electrical and Computer Engineering University of Illinois at Urbana-Champaign October 1999 +Supported by SRC, TAZ AVS99_00 TITLE AGENDA • Introduction to IMPVD • Overview of Hybrid Plasma Equipment Model • Description of sputter model • Validation of sputter model • Results and discussions for Al IMPVD • Investigating the effects of sputter heating by comparing to the results without sputter heating • Plasma properties • Depositing Al fluxes • Ar and electron densities as functions of magnetron and ICP power • Summary AVS99_01 AGENDA UNIVERSITY OF ILLINOIS OPTICAL AND DISCHARGE PHYSICS IONIZED METAL PHYSICAL VAPOR DEPOSITION (IMPVD) • Ionized Metal PVD (IMPVD) is being developed to fill deep vias and trenches for interconnect, and for deposition of seed layers and diffusion barriers. • In IMPVD, a second plasma source is used to ionize a large fraction of the the sputtered metal atoms prior to reaching the substrate. MAGNETS TARGET (Cathode) ANODE SHIELDS • 10-30 mTorr Ar buffer PLASMA INDUCTIVELY COUPLED COILS • Typical Conditions: SECONDARY PLASMA ION + NEUTRAL TARGET ATOMS Ar+ + M > Ar + M+ e + M > M+ + 2e WAFER • 100s V bias on target • 100s W - a few kW ICP • 10s V bias on substrate SUBSTRATE BIAS AVS99_02 REACTOR UNIVERSITY OF ILLINOIS OPTICAL AND DISCHARGE PHYSICS DEPOSITION PROFILES: ATOMS vs IONS • Ions are able to fill deep trenches because their spread in angles is narrowed by the rf bias. METAL ATOMS METAL IONS METAL VOID METAL SiO2 SiO2 RF BIAS AVS_03 PROFILE UNIVERSITY OF ILLINOIS OPTICAL AND DISCHARGE PHYSICS SPUTTER GAS HEATING IN IMPVD • In IMPVD processes, two types of atoms produced in the sputtering process transfer momentum and energy to background gas atoms, (sputter heating) • Sputtered metal atoms • Reflected neutral atoms produced by the incident ions • The degree of sputter heating increases with: • Magnetron power • Sputter yield • Collision cross section of the gas • This sputter heating affects • Background gas density • Ion flux to the target • Sputtered atom flux and the depositing metal flux • To investigate the effects of sputter heating, we incorporated a sputter algorithm into a Hybrid Plasma Equipment Model (HPEM). AVS99_04 INTRO UNIVERSITY OF ILLINOIS OPTICAL AND DISCHARGE PHYSICS SCHEMATIC OF 2-D/3-D HYBRID PLASMA EQUIPMENT MODEL E s (r,z) v(r,z) MAGNETOSTATICS MODULE CIRCUIT MODULE S(r,z) B(r,z) EΘ (r,z, φ ), B(r,z, φ ) I,V (coils) EΘ ELECTROMAGNETICS MODULE PLASMA CHEMISTRY MONTE CARLO SIMULATION FLUXES = 2-D ONLY ETCH PROFILE MODULE = 2-D and 3-D FLUIDKINETICS SIMULATION ELECTRON MONTE CARLO SIMULATION HYDRODYNAMICS MODULE ELECTRON BEAM MODULE ELECTRON ENERGY EQN./ BOLTZMANN MODULE NONCOLLISIONAL HEATING FDTD MICROWAVE MODULE S(r,z), T e (r,z) µ (r,z) ENERGY EQUATIONS Φ (r,z,φ ) V(rf),V(dc) Φ (r,z,φ ) R N(r,z) E (r,z, φ ) s MESOSCALE MODULE SHEATH MODULE LONG MEAN FREE PATH (SPUTTER) Φ (r,z,φ ) R σ (r,z), I (coils), J(r,z,φ ) EXTERNAL CIRCUIT MODULE SURFACE CHEMISTRY MODULE SIMPLE CIRCUIT VPEM: SENSORS, CONTROLLER, ACTUATORS SRCRM9801 AVS99_05 HPEM UNIVERSITY OF ILLINOIS OPTICAL AND DISCHARGE PHYSICS IMPROVEMENT TO SPUTTER ALGORITHMS • To better model the IMPVD process, the following improvements have been made to the sputter algorithms in the HPEM • Ion energy-dependent yield for sputtered atoms • Ion energy-dependent kinetic energy for sputtered and reflected atoms • Momentum and energy transfer from sputtered and reflected atoms to the background gas atoms • The energy-dependent yield of the sputtered atoms is* αQKs n (ε) 2.8 0.42 1− E / E ( th i ) , Ei > E th Us (1+ 0.3U s se (ε)) Y(E i ) = 0, Ei ≤ E th *Masunami et al., At. Data Nucl. Data Tables 31, 1 (1984) . • The effective yield of the reflected neutrals • 0.9 for high kinetic energy 1.2 0.8 0.4 0 0 200 400 800 Incident Ar + Energy (eV) • 0.1 for thermal energy AVS_06 IMPROVE UNIVERSITY OF ILLINOIS OPTICAL AND DISCHARGE PHYSICS ENERGY DISTRIBUTIONS OF THE SPUTTERED AND THE REFLECTED ATOMS • Energy of the emitted atoms obeys a cascade distribution: (Thompson’s law for Ei ≈ 100’s eV): 2 U UsE 21+ s , E ≤ ΛEi F(E) = ΛEi (Us + E) 3 0, E > ΛE i Us surface binding energy. ΛEi maximum recoil energy. • Reflected neutral energies are obtained from TRIM* and MD simulations. *Ar+ incident on Al, David Ruzic, Depart. of Nuclear Engineering, UIUC. • Kinetic energies of reflected neutrals are curve fitted into thermal accommodation coefficient (α) vs. incident ion energy. α= AVS_07 ENERGY Ei − Er Ei − E T • For Ar+ incident on Al target, α ≈ 0.95. UNIVERSITY OF ILLINOIS OPTICAL AND DISCHARGE PHYSICS OVERVIEW OF SPUTTER MODEL Target • The sputter model employs a kinetic Monte Carlo approach: θ • Sputter rate = Yield • (ion flux + fast neutral flux) Al Al Ar • Sputtered atoms and reflected neutrals are emitted with a cosine distribution in angle. • Collisions of sputtered atoms and reflected neutrals with the background gas are assumed to be elastic. AVS99_08 SPUTTER wafer UNIVERSITY OF ILLINOIS OPTICAL AND DISCHARGE PHYSICS OVERVIEW OF SPUTTER MODEL (Continued) • Recording of sputtered metal atoms and reflected neutrals • Thermalized Green’s Function • In-flight local density • Incorporation of statistics into fluid equations Rate of Change of Momenta and Energy Source Terms Fluid Equations Thermalized Atoms • Quantities of interest generated • Metal atom densities in the plasma • Metal flux to the wafer • Gas heating terms AVS99_09 SPUTTER2 UNIVERSITY OF ILLINOIS OPTICAL AND DISCHARGE PHYSICS MODEL VALIDATION: Al IMPVD • HPEM IMPVD model was validated by comparing with experiment (Dickson and Hopwood, J. Vac. Sci. Technol. A 15(4), 1997, p. 2307) Thermal Al Density (cm -3 ) In-Flight Al Density (cm -3 ) Target to wafer distance = 12 cm 400 W ICP 240 W Magnetron 30 mTorr Ar Al Al Target Magnet 6.0E11 Inlet • Good agreement with experimental data: Coils • V-I characteristic HPEM Voltage (V) 255 Current (A) 0.94 1.0E10 EXP. 240 1.0 1.0E8 Substrate 15 10 5 Outlet 0 RADIUS (cm) 5 10 15 • Ionization fraction of Al at r = 4 cm Distance (cm) 10 (plasma) 12 (flux) AVS99_10 VALID HPEM 15% 73% EXPERIMENT 10-15% 70% • Predicted and measured Al densities = 1011 cm-3 at r = 4 cm, 8-10 cm below target. UNIVERSITY OF ILLINOIS OPTICAL AND DISCHARGE PHYSICS SPUTTER HEATING: Ar DENSITY • Modified TEL IMPVD tool. • Operating conditions Without Sputter Heating With Sputter Heating Target to wafer distance = 15 cm • 0.5 kW ICP • 1.0 kW magnetron • 30 V rf on substrate • 30 mTorr Ar 6.8E14 Magnet Al Target Ar, cm-3 Inlet • The minimum Ar density Coils 4.6E14 • Decreases by 30% with sputter heating • Occurs below target due to sputter heating and charge exchange • Contribution to sputter heating Faraday Shield 2.5E14 Outlet Substrate 15 10 5 0 5 10 15 RADIUS (cm) • Reflected neutrals 2/3. • Sputtered metals atoms 1/3. AVS99_11 AR UNIVERSITY OF ILLINOIS OPTICAL AND DISCHARGE PHYSICS MAGNETIC FIELD, Ar+ FLUX AND DENSITY Without Sputter Heating With Sputter Heating B-field (G) 0 5 10 RADIUS (cm) 15 Ar+ (cm-3) 500 6.6E11 25 3.4E11 1 0.2E11 15 10 5 0 5 10 15 RADIUS (cm) • Exponential decay of the magnetic field away from the magnets. • The target voltage is -178 V with sputter heating, and -168 V without. • Peaks of Ar+ fluxes due to the magnetic cups. • Decreasing Ar+ density below target leads to a lower ion current and a higher voltage for the same magnetron power • Sputter heating increases the Ar+ density near the center of reactor. AVS99_12 ARPFLUX UNIVERSITY OF ILLINOIS OPTICAL AND DISCHARGE PHYSICS SPUTTER HEATING: ELECTRON TEMPERATURE Without Sputter Heating With Sputter Heating • Te(max) below the target is caused by energetic secondary electrons and joule heating. Te, eV 5.3 • Te decreases by 1 eV with sputter heating. This agrees with observations (Dickson, Qian, and Hopwood, JVST A 15 (2), 340 (1997)). 2.6 • The electron temperature is high near the coils, due to inductive heating. 0 15 10 5 0 5 10 15 RADIUS (cm) AVS99_13 TE UNIVERSITY OF ILLINOIS OPTICAL AND DISCHARGE PHYSICS SPUTTER HEATING: Al DENSITY • The maximum Al density with sputter heating is only 1/3 of that without, due to the longer mean free path. Without Sputter Heating With Sputter Heating Al, cm-3 1.7E12 • Since the magnetron power is the same, the amount of sputtered Al atoms is about equal in both cases. 4.0E10 • Sputter heating redistributes Al in the reactor to conserve the total inventory of Al atoms. 1.0E9 • The Al density with sputter heating decays much slower from the target to the substrate. 15 10 5 0 5 10 15 RADIUS (cm) AVS99_14 AL UNIVERSITY OF ILLINOIS OPTICAL AND DISCHARGE PHYSICS SPUTTER HEATING: Al+ DENSITY • The Al+ density with sputter heating has a broader peak and decreases slower toward the substrate, due to the longer mean free path in a more rarefied gas. • Note the depletion of Al+ ions by the target bias with sputter heating. With Sputter Heating Without Sputter Heating Al+, cm-3 5.2E10 6.0E9 5.0E8 15 10 5 0 5 10 15 RADIUS (cm) AVS99_15 ALP UNIVERSITY OF ILLINOIS OPTICAL AND DISCHARGE PHYSICS SPUTTER HEATING: DEPOSITING Al FLUX • The total depositing metal flux consists mostly of Al+ and thermal Al atoms . • The direct Al flux is negligible because of long throw distance (15 cm, ~10 mfp), and Al* is depleted by ionization. • The magnitude of the Al flux with sputter heating is >2 times that without, while the ionization fraction decreases to 67-86% from above 90%. • Without sputter heating • With sputter heating 3 3 Total 2 2 Al+ Total 1 1 Thermal Al Al+ 0 0 2 4 6 Radius (cm) AVS99_16 AL_FLUX 8 10 Thermal Al 0 0 2 4 6 8 10 Radius (cm) UNIVERSITY OF ILLINOIS OPTICAL AND DISCHARGE PHYSICS Ar DENSITIES vs MAGNETRON AND ICP POWER • Both the minimum and the reactor averaged Ar densities decrease with increasing magnetron power due to increasing sputter heating. • The minimum Ar densities converge at high magnetron power • The specific power density decreases due to longer stopping distance. • The minimum gas density occurs right below the target, and the heat loss to the target increases as the gas temperature increases. • Ar - Minimum 5 • Ar - Average 5 0.5 kW ICP 4 4 0.5 kW ICP 1.0 kW 3 2 1.0 kW 3 1.5 kW 2 1.5 kW 1 1 0 0 0.5 1.0 1.5 Magnetron Power (kW) AVS99_17 POWER 2.0 0 0 0.5 1.0 1.5 2.0 Magnetron Power (kW) UNIVERSITY OF ILLINOIS OPTICAL AND DISCHARGE PHYSICS ELECTRON DENSITY vs MAGNETRON AND ICP POWER • The electron density significantly increases when magnetron power is increased from zero due to low-ionization potential metal atoms . • As the magnetron power further increases, the electron density saturates due to decreasing Al ionization fraction. • At constant magnetron power, electron density increases linearly with ICP power. 8 1.5 kW 6 1.0 kW • Average electron density 4 0.5 kW ICP 2 0 0 0.5 1.0 1.5 2.0 Magnetron Power (kW) AVS99_18 POWER_E UNIVERSITY OF ILLINOIS OPTICAL AND DISCHARGE PHYSICS SUMMARY OF SPUTTER HEATING STUDY • Sputter heating from both sputtered metal atoms and reflected neutrals significantly rarefies the background gas, thus increasing the mean free path for transport of the sputtered atoms and redistributing metal species in the reactor. • Sputter heating decreases the ionization fraction of the depositing metal flux, but increases its magnitude, similar to operating at lower pressure. • Sputter heating should NOT be neglected in the modeling of IMPVD processes. • The addition of small amount of metal atoms with low ionization potential significantly increases the electron density. • Electron density tends to saturate with increasing magnetron power since gas rarefaction reduces the ionization fraction of the metal atoms. AVS99_19 CONCLU UNIVERSITY OF ILLINOIS OPTICAL AND DISCHARGE PHYSICS
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