Dr. Sabrina Lee and Dr. Rong Wei NDIA Gun and Missile Conference, New Orleans, LA April 21-24, 2008

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Weapon Systems & Technology Directorate US ARMY ARDEC- BENÉT LABS TITLE: PLASMA ENHANCED MAGNETRON TECHNOLOGY FOR DURABLE POLLUTION-FREE COATINGS Dr. Sabrina Lee and Dr. Rong Wei NDIA Gun and Missile Conference, New Orleans, LA April 21-24, 2008

Outline Problems with HC Cr electroplating process. Alternative pollution-free coatings against high temperature wear and erosion. Plasma enhanced magnetron surface cleaning. Plasma enhanced magnetron deposition. Analytic characterization and adhesion testing. Conclusion 2

Problems with Electroplated Cr Environment Problem: Aqueous toxic Cr VI from Cr Electroplating Process Performance Problem: Inadequate substrate protection, reduced service life for high temp wear & erosion applications 3

Plasma Enhanced Magnetron Sputtering Conventional Physical Vapor Deposition via DC Magnetron Sputtering Plasma Enhanced Magnetron Sputtering with Filament and Biasing at SwRI Magnetron Magnetron Generated Plasma Power Supply Samples - - Worktable Power Supply Ar,N2 To Pump Filament Plasma + Magnetron Plasma Current Density ~ 4.9 ma/cm 2 Magnetron Plasma without Filament Plasma Current Density ~ 0.2 ma/cm 2 4

Planned Plasma Enhanced Cylindrical Magnetron Deposition RF Power Supply - Magnetron Power Supply Magnetron Rectangular Magnets Target Coating Gun Barrel Vacuum Chamber - Bias Power Supply LEFT- MIDDLE- RIGHT- RF-plasma enhanced cylindrical magnetron sputtering experiments at SWRI. HIPIMS (high power impulse magnetron sputtering) from- Dr. J. Bohlmark, Dr. J. Alami. ARDEC-Benet Labs CMS platforms for coating full-length 120mm large cal bore. 5

Potential Applications of Technology 6

Properties of Ta, Cr, A723 Gun Steel Properties Steel Cr α-ta Melting Point Temperature [ C] 1535 1857 2996 Lattice Parameter* [Angstroms] 2.8665 2.8847 3.298 Lattice Mismatch with alpha Fe -0.6% -15.1% Lattice Mismatch with alpha Ta 13.1% 12.5% Thermal expansion at RT (K-1)** 1.35E-05 6.50E-06 6.50E-06 Difference in thermal expansion with Fe 51.9% 51.9% thermal conductivity, k [W/mK]*** 45.1 98.5 57.7 Young's Modulus, E (GPa)**** 207 248 173 *Cullity **Smithell's 6th Ed. ***Underwood; Incorpera & DeWitt, Introduction to Heat Transfer ****Thornton & Colangelo, Fundamentals of Engineering Materials 7

Properties of bcc and tetragonal Ta α-ta β-ta Structure BCC Tetragonal Lattice Parameters a=b=c= 0.33058 nm a=b=1.0194 nm c=0.5313 nm Hardness 100-200 KHN 1000-1200 KHN Resistivity 15-60 μω-cm 200 μω-cm Thermal Stability T m = 2996 o C T β α ~ 750 o C Ductility Ductile Brittle 2-Theta Random α Ta (110) (left ring) Random β Ta (002) (right ring) Chi softer bcc Ta on Steel harder tetragonal Ta on steel Random α Ta (110) (left ring) Textured β Ta (002) (right ring) 8

Sputter Cleaning of Gun Steel Native oxide on gun steel surface is ~10-20 nm Heat-Generated (350ºC for 3 hrs in air) oxide is ~300-350 nm. AES showed ion sputter cleaning for 60 min removed all native and heat-induced oxides. 50 Surface Oxide of Gun Steel Oxygen Concentration (at%) 45 40 35 30 25 20 15 10 5 0 "Native" Oxide Oxidized at 350 C for 3 hours 0 100 200 300 400 500 600 AES Sputtering Time (sec) 9

Sputtered Cr on A723 Gun Steel Higher discharge current increases hardness, density, improves microstructure 0A, 14 µm, 85 min, HK 10 399 5A, 13 µm, 85 min, HK 10 633 10A, 13 µm, 85 min HK 10 1226 20A, 6 µm, 90 min, HK 10 2144 10

Sputtered Ta on A723 Gun Steel Higher discharge current increases hardness, density, residual stresses, α-ta formation Ta 4 Ta 5 Ta 13-15 Ta 4 Ta 5 Ta 13-15 10A, 90µm, 600 min HK 10 602, α-ta 0A, 10µm, 60 min HK 10 552, (α+β)-ta 10A, 148µm, 900 min, HK 10 337, α-ta 11

Sputtered Ta on Rifled 155mm Plasma Enhanced DC Magnetron Coating Topography Land-Groove, 450 micron Ta Walls- 250 micron Ta Plasma Enhanced DC Magnetron Coating Microstructure Land-Groove, 450 micron Ta Walls- 250 micron Ta HIPIMS (High Intensity Impulse Magnetron Sputtering) (Helmersson/Rhode/Lee) Uniform 2 micron bcc Ta on slanted edge of gun steel sample 12

Coatings Adhesion Testing Microscratch Test of Thin Coatings Groove Test (ASTM B571-91) Pulsed Laser Heat Test Vented Erosion Simulator Test (In-Door Firing Range) Laser Optical Fiber Tungsten carbide tool Direction of groove Coating Surface Groove Test for Coatings Adhesion Strength (a) Vented Erosion Simulator Combustion Chamber Groove Gas Adhesion Gas Testing Inlet Outlet Burst Disk High P, T, & h Sample Thermocouple Temperature vs. Time PLH (Pulsed Laser Heating) Test of Thermal Properties of Coatings (b) Sample Insert Sample Insert Coating Surface VES (Vented Erosion Simulator) Test of Thermal-Mechanical- Chemical Properties of Coatings 13

Electroplated Cr Groove Adhesion Testing (ASTM B571-91) Cr16 Cr24 Cr 15 Ta3 Ta12-2 Ta13-15 Cohesive failures 155mm Land 155mm Groove 14

Internal Ballistic and Transient Thermal Simulation 120mm Cannon Firing and Pulsed Laser Heating surface temp (K) 3500.0 3000.0 2500.0 2000.0 1500.0 1000.0 cannon, 0.6 m cannon, 1.6 m 1 ms, 1 J/mm^2 1 ms, 0.5 J/mm^2 2.5 ms, 1 J/mm^2 500.0 0.0 0.E+00 1.E-03 2.E-03 3.E-03 4.E-03 5.E-03 6.E-03 time (s) 15

Comparative Pulsed Laser Heating Tests PLH parameters (2.5 msec, 1.0 J/mm2, 20 cycles, simulating ~1480 C temperature) 90 μm Sputtered bcc Ta in Ar on Steel (Ta4) Ta HAZ Steel 80 μm Sputtered bcc Ta in Kr on Steel (Ta 12-2) Ta HAZ Steel 125 μm Electroplated Cr on Steel (Cr-1966-01) Cr Steel HAZ HAZ (Heat affected zone) in steel is due to tempered to untempered martensite transformation. During heating-cooling cycle, martensite transforms to austenite, then back to martensite 16

148μm Ta on Gun Steel after 25 VES Firing High Erosive RDS Axial (1.0 inch from end of 1.6 inch long sample) After 25 rounds Axial hardness Axial oxide layer As deposited As-deposited topography - microstructure After fired surface Minimal softening, good adhesion, no cracking after 25 VES rds! 17

286μm Ta on Steel After 129 VES Firing High Erosive RDS Longitudinal Ta Thickness = 204 µm Transverse Ta Thickness = 203 µms Minimal softening, good adhesion, no cracking after 129 VES rds! 18

VES Firing Comparison: Electroplated Cr vs. Plasma Enhanced Sputtered Ta Plasma Enhanced bcc Ta (286µm) on steel after 129 cycles VES high erosive rds Showing excellent structure, adhesion, and crack-resistance properties Electroplated HC Cr (120µm) on Steel ~ 100 cycles of VES under same conditions Electroplated HC Cr (120µm) on Steel ~100 cycles of actual firing of high erosive rds 19

Conclusions 1) Plasma enhanced magnetron technology using higher ion bombardment can deposit hard, dense, adhesive, pollution-free coatings on steel with improved microstructure. 2) Plasma enhanced sputtered Ta on 120mm and 155mm test samples demonstrated excellent structure, ductility, adhesion, and resistance against thermal shock cracking and high temperature erosion. 3) Plasma enhanced sputtered Ta has potential to coat 120mm and 155mm barrels and other armament components, with expected improved cycle life due to the high melting point temperature and absence of cracks. 20