GA A22869 BOUNCE COATING INDUCED DOMES ON GLOW DISCHARGE POLYMER COATED SHELLS

Similar documents
GA A23757 COATING AND MANDREL EFFECTS ON FABRICATION OF GLOW DISCHARGE POLYMER NIF SCALE INDIRECT DRIVE CAPSULES

ENLARGEMENT OF GLASS AND PLASTIC SHELLS TO 2 mm IN DIAMETER BY REDROPPING THROUGH A SHORT HEATED TOWER

Performance of Smoothing by Spectral Dispersion (SSD) with Frequency Conversion on the Beamlet Laser for the National Ignition Facility

GA A22583 FAST WAVE ANTENNA ARRAY FEED CIRCUITS TOLERANT OF TIME-VARYING LOADING FOR DIII D

GA A22712 DIII D ICRF HIGH VOLTAGE POWER SUPPLY REGULATOR UPGRADE

GA A25836 PRE-IONIZATION EXPERIMENTS IN THE DIII-D TOKAMAK USING X-MODE SECOND HARMONIC ELECTRON CYCLOTRON HEATING

GA A22897 QUASI-OPTIC COMPONENTS IN OVERSIZED CORRUGATED WAVEGUIDE FOR MILLIMETER-WAVE TRANSMISSION SYSTEMS

GA A27238 MEASUREMENT OF DEUTERIUM ION TOROIDAL ROTATION AND COMPARISON TO NEOCLASSICAL THEORY IN THE DIII-D TOKAMAK

A REGULATED POWER SUPPLY FOR THE FILAMENTS OF A HIGH POWER GYROTRON

INFRARED MEASUREMENTS OF THE SYNTHETIC DIAMOND WINDOW OF A 110 GHz HIGH POWER GYROTRON

GA A22574 ADVANTAGES OF TRAVELING WAVE RESONANT ANTENNAS FOR FAST WAVE HEATING SYSTEMS

Preparation of Random Phase Plates for Laser Beam Smoothing

INITIAL RESULTS FROM THE MULTI-MEGAWATT 110 GHz ECH SYSTEM FOR THE DIII D TOKAMAK

GA A FABRICATION OF A 35 GHz WAVEGUIDE TWT CIRCUIT USING RAPID PROTOTYPE TECHNIQUES by J.P. ANDERSON, R. OUEDRAOGO, and D.

THE MEASURED PERFORMANCE OF A 170 GHz REMOTE STEERING LAUNCHER

Quarterly Technical Progress Report. For the period starting July, , ending September 30, Xiaodi Huang and Richard Gertsch

AN IN-LINE POWER MONITOR FOR HE11 LOW LOSS TRANSMISSION LINES

Sandia National Laboratories MS 1153, PO 5800, Albuquerque, NM Phone: , Fax: ,

GA A22577 AN ELM-RESILIENT RF ARC DETECTION SYSTEM FOR DIII D BASED ON ELECTROMAGNETIC AND SOUND EMISSIONS FROM THE ARC

Nanosecond, pulsed, frequency-modulated optical parametric oscillator

GA A22776 THE DESIGN AND PERFORMANCE OF WAVEGUIDE TRANSMISSION LINE COMPONENTS FOR PLASMA ELECTRON CYCLOTRON HEATING (ECH) SYSTEMS

Microsecond-long Lasing Delays in Thin P-clad InGaAs QW Lasers

Implementation of an Acoustic Emission Proximity Detector for Use in Generating Glass Optics. M. A. Piscotty, J. S. Taylor, K. L.

Performance of Keck Adaptive Optics with Sodium Laser Guide Stars

AN ELM=RESlLlENT RF ARC DETECTION SYSTEM FOR DIII-D BASED ON ELECTROMAGNETIC AND SOUND EMISSIONS FROM THE ARC

GA A26816 DESIGNS OF NEW COMPONENTS FOR ITER ECH&CD TRANSMISSION LINES

UCRL-ID Broad-Band Characterization of the Complex Permittivity and Permeability of Materials. Carlos A. Avalle

Defect Study in Fused Silica using Near Field Scanning Optical Microscopy

Accelerator and Fusion Research Division Lawrence Berkeley Laboratory University of California Berkeley, CA 94720

HIGH-POWER CORRUGATED WAVEGUIDE COMPONENTS FOR mm-wave FUSION HEATING SYSTEMS

Evaluation of Roof Bolting Requirements Based on In-Mine Roof Bolter Drilling

The Development of an Enhanced Strain Measurement Device to Support Testing of Radioactive Material Packages*

Five-beam Fabry-Perot velocimeter

PERFORMANCE OF THE 110 GHz SYSTEM ON THE DIII D TOKAMAK

&wf-9+/ob/--21*~~ II. Ron Harper and Robert A. Hike

Recent advances in ALAMO

Up-conversion Time Microscope Demonstrates 103x Magnification of an Ultrafast Waveforms with 300 fs Resolution. C. V. Bennett B. H.

FAST WAVE ANTENNA ARRAY FEED CIRCUITS TOLERANT OF TIMElVARYING LOADING FOR DIII-D

Cascaded Wavelength Division Multiplexing for Byte-Wide Optical Interconnects

RF HIGH VOLTAGE PERFORMANCE OF RF TRANSMISSION LINE COMPONENTS ON THE DIII-D FAST WAVE CURRENT DRIVE (FWCD) SYSTEM

The ACT External HEPA Push-Through Filter Assembly. A. A. Frigo, S. G. Wiedmeyer, D. E. Preuss, E. F. Bielick, and R. F. Malecha

Developing Enabling Optics Finishing Technologies for the National Ignition Facility

GA A23281 EXTENDING DIII D NEUTRAL BEAM MODULATED OPERATIONS WITH A CAMAC BASED TOTAL ON TIME INTERLOCK

GA A23983 AN ADVANCED COLLABORATIVE ENVIRONMENT TO ENHANCE MAGNETIC FUSION RESEARCH

Measurements of MeV Photon Flashes in Petawatt Laser Experiments

Determination and Correction of Optical Distortion in Cryogenic Target Characterization

Image Enhancement by Edge-Preserving Filtering

National Accelerator Laboratory

SHADOWGRAPH ILLUMINIATION TECHNIQUES FOR FRAMING CAMERAS

Spatial Frequency Domain Error Budget. Debbie Krulewich and Herman Hauschildt

High Explosive Radio Telemetry System. Federal Manufacturing & Technologies. R. Johnson, FM&T; B. Mclaughlin, FM&T;

GA A24030 ECE RADIOMETER UPGRADE ON THE DIII D TOKAMAK

GA A23741 DATA MANAGEMENT, CODE DEPLOYMENT, AND SCIENTIFIC VISUALIZATION TO ENHANCE SCIENTIFIC DISCOVERY THROUGH ADVANCED COMPUTING

MAPPING INDUCED POLARIZATION WITH NATURAL ELECTROMAGNETIC FIELDS FOR EXPLORATION AND RESOURCES CHARACTERIZATION BY THE MINING INDUSTRY

Evaluation of Confocal Microscopy. for Measurement of the Roughness of Deuterium Ice. Ryan Menezes. Webster Schroeder High School.

National Accelerator LaboratoryFERMILAB-TM-1966

Argonne National Laboratory P.O. Box 2528 Idaho Falls, ID

U.S.Department of Energy

Detector And Front-End Electronics Of A Fissile Mass Flow Monitoring System

THE 110 GHz MICROWAVE HEATING SYSTEM ON THE DIII D TOKAMAK

Stimulated Emission from Semiconductor Microcavities

AIGaAs/InGaAIP Tunnel Junctions for Multifunction Solar Cells. Sharps, N. Y. Li, J. S. Hills, and H. Hou EMCORE Photovoltaics

DESIGNING MICROELECTROMECHANICAL SYSTEMS-ON-A-CHIP IN A 5-LEVEL SURF ACE MICROMACHINE TECHNOLOGY

Observation of amplification of a 1ps pulse by SRS of a 1 ns pulse in a plasma with conditions relevant to pulse compression

High-]FrequencyElectric Field Measurement Using a Toroidal Antenna

GA A25824 A NEW OVERCURRENT PROTECTION SYSTEM FOR THE DIII-D FIELD SHAPING COILS

GA A26150 PROGRESS ON DESIGN AND TESTING OF CORRUGATED WAVEGUIDE COMPONENTS SUITABLE FOR ITER ECH AND CD TRANSMISSION LINES

Armlication For United States Patent For HOT CELL SHIELD PLUG EXTRACTION APPARATUS. Philip A. Knapp Moore, ID. and. Larry K. Manhart Pingree, ID

Laser Surface Profiler

Measurements of edge density profile modifications during IBW on TFTR

GA A SOLID-STATE HIGH VOLTAGE MODULATOR WITH OUTPUT CONTROL UTILIZING SERIES-CONNECTED IGBTs by J.F. TOOKER and P. HUYNH

MASTER --3. Gtl.- DISTRIBUTION. THiS DOCUMENT IS UNLIMITED PNL-SA Shaw Whiteman Anderson Alzheimer G. A. March 1995

AN OVERVIEW OF THE TARGET FABRICATION OPERATIONS AT LAWRENCE LIVERMORE NATIONAL LABORATORY

Final. NO.Report CRADA. Date: September 11, 1997

+o GENEML ATOMfCS. RF POWER DIAGNOSTICS AND CONTROL ON THE DIII-D, 4 MW MHz FAST WAVE CURRENT DRIVE SYSTEM (FWCD)

by T.E. HARRIS, J.C. ALLEN, W.P. CARY, S.W. FERGUSON,* C.C. PETTY, and R.I. PINSKER

STP-PT-032 BUCKLING OF CYLINDRICAL, THIN WALL, TRAILER TRUCK TANKS AND ASME SECTION XII

Radio Frequency Current Drive for Small Aspect Ratio Tori

Supporting Information 1. Experimental

AFM Study of Hydrocarbon Thin Films

Introduction to Radar Systems. The Radar Equation. MIT Lincoln Laboratory _P_1Y.ppt ODonnell

Detection of Targets in Noise and Pulse Compression Techniques

A Laser-Based Thin-Film Growth Monitor

Parasitic Pencil Beams Caused by Lens Reflections in Laser Amplifier Chains

MAPPING INDUCED POLARIZATION WITH NATURAL ELECTROMAGNETIC FIELDS FOR EXPLORATION AND RESOURCES CHARACTERIZATION BY THE MINING INDUSTRY

Lawrence Berkeley National Laboratory Recent Work

' Institut fuer Kernphysik, Strahlenzentrum, JLU Giessen, Germany 3

k SLAC-PUB-7583 July 1997 Co/vF PULSE TRANSFORMER R&D FOR NLC KLYSTRON PULSE MODULATOR*

STP-PT-054 CONCENTRATED SOLAR POWER (CSP) CODES AND STANDARDS GAP ANALYSIS

Assisting DOE EM 4.12, Office of Groundwater and Subsurface Closure

A Project Report Submitted to the Faculty of the Graduate School of the University of Minnesota By

Standard Operating Procedure of Atomic Force Microscope (Anasys afm+)

Fabrication of a submicron patterned using an electrospun single fiber as mask. Author(s)Ishii, Yuya; Sakai, Heisuke; Murata,

National Accelerator Laboratory

IMU integration into Sensor suite for Inspection of H-Canyon

A Novel Way to Characterize Metal-Insulator-Metal Devices via Nanoindentation

Giovanni P. Donati - MST-11 Daniel Some - MST-11 George Rodriguez - MST-11 Antoinette J. Taylor - MST-11

PEP-I11Magnet Power Conversion Systems:.

IMPACT TESTING EXEMPTION CURVES

Infra-Red Propagation Through Various Waveguide Inner Surface Geometries

Transcription:

GA A22869 BOUNCE COATING INDUCED DOMES ON GLOW DISCHARGE by A. NIKROO and D. WOODHOUSE JUNE 1998

DISCLAIMER This report was prepared as an account of work sponsored by an agency of the United States Government. Neither the United States Government nor any agency thereof, nor any of their employees, makes any warranty, express or implied, or assumes any legal liability or responsibility for the accuracy, completeness, or usefulness of any information, apparatus, product, or process disclosed, or represents that its use would not infringe privately owned rights. Reference herein to any specific commercial product, process, or service by trade name, trademark, manufacturer, or otherwise, does not necessarily constitute or imply its endorsement, recommendation, or favoring by the United States Government or any agency thereof. The views and opinions of authors expressed herein do not necessarily state or reflect those of the United States Government or any agency thereof.

GA A22869 BOUNCE COATING INDUCED DOMES ON GLOW DISCHARGE by A. NIKROO and D. WOODHOUSE This is a preprint of a paper to be presented at the 12th Target Fabrication Specialists Meeting, April 19 23, 1998, Jackson Hole, Wyoming and to be published in Fusion Technology. Work supported by the U.S. Department of Energy under Contract No. DE-AC03-95SF20732 GA PROJECT 3748 JUNE 1998

BOUNCE COATING INDUCED DOMES ON GLOW DISCHARGE A. NIKROO AND D. WOODHOUSE BOUNCE COATING INDUCED DOMES ON GLOW DISCHARGE A. Nikroo and D. Woodhouse Inertial Fusion Division, General Atomics PO Box 85608 San Diego, CA 92186-5608 (619) 455-2931 ABSTRACT Plasma polymer coating of larger (1 mm or greater in diameter) Inertial Confinement Fusion (ICF) targets in a piezo electric based bounce pan results in surfaces which contain numerous domes of various sizes for coating thicknesses greater than about 3 µm. The density of domes increases with the size of the shells, number of shells coated at once, the strength of bouncing, and the coating thickness. The same problem is encountered when bounce coating large numbers of smaller Nova shells as well. The domes appear to grow from seeds produced by chips of the brittle plasma polymer coating itself produced in shell-toshell collisions. A tilted spinning pan has been shown to produce smooth dome free coating while providing sufficient agitation to obtain uniform coatings. I. INTRODUCTION ICF target shells generally contain an ablator layer which is mainly a glow discharge polymer (GDP) film deposited by plasma polymeriazation. 1 The surface finish of the finished ICF targets must satisfy demanding specifications. Such specifications are normally provided by an ideal modal power spectrum. 2 For uniform deposition of the GDP layer, the spherical targets must be agitated during coating. A piezo electric driven bounce pan has been used extensively and with great success for this purpose on Nova size (440 µm diameter) shells. 1,3 In the our laboratory's production environment, coating a large number of shells at the same time is required in order to provide timely turn around on the requested targets. We have encountered a problem in using the piezo bouncing system when coating large numbers of various types of shells. Frequent collisions between the shells during the coating results in dome filled surface finishes for the shells and production of small beads during the coating. We report here on the correlation between the density of domes on the GDP surfaces and the number, size and agitation strength of shells in the piezo bouncing scheme. We also show that a tilted spinning pan is superior to the piezo bouncer for large scale production GDP coatings. This agitation scheme reduces the collisions between the shells and results in the improved surfaces for the finished targets. The origin of domes is also discussed. II. EXPERIMENTAL All mandrels used for the experiments were PAMS mandrels made by the droplet generator technique. 4 The plasma polymerization system based on a helical resonator and the piezo bouncer have been described elsewhere by other authors. 1,5 Our coaters are clones of such a system. These systems are routinely used for deposition of ablator layers for experiments at various ICF laboratories. 6 For the rotating pan agitation, a small DC motor capable of being operated in vacuum and in a plasma was fitted with a gear reduction head and was used to spin the coating pan at 0.2 to 3 Hz. The spinning pan was mounted with approximately a 15 tilt to vertical on a rod through a vacuum feedthrough to allow tapping the pan to dislodge stuck shells. The surface finish of the shells was examined optically and by Scanning Electron Microscopy SEM) and spheremapper atomic force microscope (AFM). III. RESULTS We have found very dome filled surfaces after GDP coating of pristine OMEGA size PAMS mandrels [Fig. 1(a)] when the shells are vigorously bounced in a piezo based bouncer. Coatings of 3 µm or less exhibit very GENERAL ATOMICS REPORT GA-A22869 1

A. NIKROO AND D. WOODHOUSE BOUNCE COATING INDUCED DOMES ON GLOW DISCHARGE (a) (b) Fig. 1. (a) Scanning electrom microscope (SEM) image of the surface of a 12 µm coating of GDP on an OMEGA (900 µm) size PAMs mandrel. The surface contains numerous domes. This shell is one of 120 shells bounced coated together at once. The bouncing action was very vigorous in order to obtain a uniform GDP coating on the non-uniform PAMs mandrel. A bead can be seen near the lower right hand side of the image. (b) A side view of the surface of another shell exhibiting many domes on the surface. The presence of beads along with the domes is clearly seen in this view. The scale bars are 10 µm.the beads in (b) are about 10 µm tall. few domes, while once the thickness is above 4 µm the surface becomes filled with domes. The density of domes increases as the thickness increases. In addition, spherical beads of about 10 µm diameter are usually seen attached to the shells [Fig. 1(b)]. The beads can be washed or knocked off the shells and are therefore not integrated into the coating. The background surface finish, however, is the usual 1 or less nm RMS. 5 The domes result in power increase in the modal spectrum of the shell as examined by the spheremapper AFM (Fig. 2). While the main contribution of the domes is to modes greater than 100, there is a significant increase in the power in modes 10 100. In particular, mode 100 power is almost one order of magnitude higher on the GDP coated shells. This enhacement of middle modes power can be very important for larger, 2 mm, National Ignition Facility (NIF) targets, and is believed to be critical for NIF target performance. We set out to determine the cause of such poor surface finishes. These types of surface finishes were found in three different independent coating systems, with the problem occuring intermittently. Uncleanliness of the systems or feed gases is usually suspected when such surface finishes are encountered. All systems were carefully cleaned but the problem persisted. To examine possible cause of this problem, we performed a set of systematic experiments. We deposited about 10 µm of GDP on various substrates. The coated surfaces contained a large number of domes only when a large number of shells (100 or more) were coated together. Coatings on flats or on small number of shell were virtually dome free. The original PAMS mandrels were all chosen to have very clean Power, nm 2 10 5 10 4 10 3 10 2 10 1 10 0 10 1 10 2 10 3 Dome free coating 1 10 100 1000 Wave-number Power increase due to domes Fig. 2. Spheremapper AFM traces of OMEGA sized bare PAMS mandrels (thin line) and GDP coated PAMS mandrels (thick line). The density of domes on the GDP surface was similar to that in Fig. 1(a). Each trace is an average of two shells. The surface domes contribute to the modal spectrum mainly in the modes greater than 100, but they also result in significant power in the critical 10 100 mode range as well. surfaces. Thus, there appeared to be a correlation between the number of shells coated and the surface finish. The shells were bounced very vigorously in all of these runs in order to correct for the non-concentricity of the original PAMS mandrels. Gentle bouncing of a large number of shells was tried next. While the surface still contained numerous domes, the dome density was far lower than when the shells were bounced vigorously. In a number of 2 GENERAL ATOMICS REPORT GA-A22869

BOUNCE COATING INDUCED DOMES ON GLOW DISCHARGE the deposition runs a few shells were placed on stationary holder near the plasma tube away from the bounce pan. While the shells bounced in the pan had very poor surfaces, the coatings on the stationary shells were virtually dome free. Therefore, vigorous bouncing of large numbers of shells was creating seeds for domes observed on the surface. Shells of different diameters were bounce coated both vigorously and gently in large and small batches in separate coating runs to further examine the process. Results simliar to coating of OMEGA shells were obtained with Nova size, NIF size and 1.6 mm diameter shells. If too many shells were coated together, the final surface contained many domes. The density of domes increased as the shells were bounced more vigorously. While the surface finish improved as the bouncing strength was reduced, the coatings became more and more non-uniform. It was not possible to coat a large number of shells and obtain a uniform coating free of domes. A sample of the results is shown in Fig. 3. The results for the spinning pan agitation mechanism is also shown for comparison and will be discussed later. For the same bouncing agitation, the difference for each size is the maximum number of shells, n-max, that can be coated together without having a dome filled finished surface. n-max becomes smaller as the diameter of the shells increases. In particular, it appears that n-max varies as the inverse of the fifth power the diameter. This rather steep dependence may be plausible when one considers that the frequency of shell to shell collisions rises rapidly as the diameter of the Domes/unit area 300 250 200 150 100 50 Bounced hard, n > n max Bounced hard, n < n max Rolled, n > n max 0 0 500 1000 1500 2000 Shell Diameter, µm Fig. 3. Number of domes on the final GDP surface for bounce coating shells of different diameters to a nominal thickness of 12 µm. n is the number of shells bounced in the coating pan. n-max is the maximum number that can be vigourously bounced ( bounced hard ) together while resulting in only a relatively small number of domes on the GDP surface. When the shells are rolled, a virtually dome free surface is obtained even when coating large numbers of shells together. A. NIKROO AND D. WOODHOUSE shells (and at the same time the mass of the shells) increases. As in case of OMEGA size shells, gentle bouncing improved the surface of all types of shells but the agitation was not enough for the larger shells. In particular, the coating on gently bounced NIF size shells is very non-uniform (non-concentricity = 25%). IV. ALTERNATIVE BOUNCING TECHNIQUES The problem of using a piezo based shaker to coat larger size PAMS shells has been encountered previouly by Saculla et. al. 7 A pan mounted on a swaying rod driven by a mechanical shaker had improved the surface finish in their case. We have found a dramatic reduction in the number of domes if the larger (OMEGA size and larger) shells are coated in a spinning tilted pan. A 15 tilt angle was enough to cause constant agitation of the shells without any sticking problems when the pan was spun at approximately 60 revolutions per minute (RPM). The spinning action of the pan keeps the shells agitated while reducing the probability of collisions between shells. The shells in effect keep chasing each other in this configuration instead of running into each other as in the piezo shaker setup. At the beginning of a given coating run, many shells usually stick to the pan and the tapper rod is used to knock these shells loose. After the shells receive a small amount of coating they roll freely without sticking. Figure 4 shows the reduction of the density of domes when this agitation mechanism is used as opposed to bounce coating shells rather vigorously. Twelve NIF size shells were coated in each case. The shells coated using the piezo bouncer agitation has a very dome filled surface, while those coated in the spinning pan were virtually dome free. With this agitation scheme we were able to coat over 100 OMEGA size shells with virtually dome free surface. The major concern in rolling agitation was the possible non-uniform coating of the shells due to insufficient agitation. We examined this by coating PAMS mandrels with very good average non-concentricity (NC) of less than 5%. The resulting GDP mandrels also had a NC of less than 5% indicating uniform coating of the mandrels in the rolling pan. V. ORIGIN OF DOMES The diameter of a dome is related to the coating thickness and the diameter of the seed particle. 1,8 The seeds result in cone like growths within the coating as the coating thickness increases. Because of the nonhomogeneity in the size of the surface domes, either the seeds must be of different sizes or the seeds must have attached themselves to the shells at different times during the coating. SEM cross-sectional examination was used for examination of this type of growth. We chose highly GENERAL ATOMICS REPORT GA-A22869 3

A. NIKROO AND D. WOODHOUSE BOUNCE COATING INDUCED DOMES ON GLOW DISCHARGE (a) (b) Fig. 4. (a) The surface of a 2 mm PAMs shell coated with 12 µm of GDP in a bounce pan. The surface is littered with domes. (b) A similar PAMs mandrel coated in the rolling pan with 12 µm of GDP. The surface is virtually dome free, while coating thickness was very uniform around the shell. 12 shells were coated together in each case. dome filled surfaces of NIF sized shells to minimize the search for domes in the SEM. Figure 5 shows a cross-section of the such a shell. The predicted cone like growth of the domes is clearly visible. It is interesting to note that the origin of the domes is not at the inner surface, but rather is in general 2 to 3 µm above the inner the surface. This is consistent with the lack of domes on coating of 3 µm or less. Therefore, it appears that the seeds are produced by the abrasion of the GDP coating, and not the PAMS mandrels. This was further supported by vigorous bouncing of a large number of OMEGA size PAMS in a pan in the absence of any GDP. The surface of the shells did not deteriorate in the process. The chipping of the GDP coating and not the original PAMS in hard collisions between shells may result from an increase in brittleness of thicker coatings. Despite, this evidence more tests have to be done to verify this hypothesis for the origin of seeds for the domes. Start of coating Fig. 5. SEM cross-section of an approximately 2 mm bounce coated GDP shell made by the depolymerizable technique. The cone-like growth of domes is easily apparent. However, it appears that none of the cones extends all the way to the start of the coating. The deepest cones seem to originate at a coating thickness of 2 to 3 µm. This is consistent with the observation that coatings thinner than 3 µm do not have dome filled surfaces. VI. CONCLUSION While the piezo bouncing system has been extremely successful in coating smaller Nova targets, it appears to have major limitations for coating 1 mm or larger shells. This is especially true in the production environment where larger numbers of shells have to be coated together. The larger diameters of the OMEGA and NIF targets result in increased collisions between the targets in the piezo bouncing scheme, leading to very dome-filled coatings. A tilted spinning pan has been shown to provide sufficient agitation of shells for uniform coatings, while producing virtually dome free surfaces. ACKNOWLEDGMENT Work supported by U.S. Department of Energy under Contract No. DE-AC03-95SF20732. REFERENCES 1. S.A. Letts, et al., J. Vac. Sci. Technol. 19, 739 (1981). 2. R.L. McEachern, et al., J. Vac. Sci. Technol. A 13, 983 (1995). 3. W.L. Johnson, et al., Plasma Polymerization, M. Shen and A.T. Bell, Eds. (American chemical Society, Washington, DC, 1979). 4. B.W. McQuillan, et al., Fusion Tech., 31, 381 (1997). 5. S.W. Ferguson, et al., J. of Applied Polymer Science, 54, (1994) p.107. 6. A. Nikroo, et al., Proc. 11th Target Fabrication Specialists' Meeting, Orcas Island, Washington (1996). 7. M. Saculla, S.A. Letts, Proc. 11th Target Fabrication Specialists' Meeting, Orcas Island, Washington (1996). 8. R.C.Cook, Laser Program Target Science and Technology, Lawrence Livermore National Laboratory, Livermore, CA, internal memo TST92-047 (1992). 4 GENERAL ATOMICS REPORT GA-A22869