Optics and Laser Heads for Laser-Interferometer Positioning Systems Product Overview Choose from a large selection of optical components for system design flexibility Table of Contents 3 4 6 8 8 9 10 12 14 22 23 24 26 28 Design Your System for Peak Performance Laser Head Specifications Directing Optics Specifications Measurement Optics Specifications Linear Optics Single Beam Optics Plane Mirror Optics Differential Interferometer Multiaxis Optics Wavelength Tracker Accessory Specifications Receiver Specifications Optics and Laser Head Configuration Guide Example Configurations How to Use This Product Overview This product overview provides details on the laser heads, receivers, and optics used by all Agilent Technologies laser interferometer positioning systems. Together with the electronics information contained in companion data sheets, this information will enable you to specify your entire laser positioning system. Select from the following companion data sheets: * Agilent 5527B Laser Interferometer Positioning System * High Performance Laser Interferometer Positioning Systems for VMEbus * Complete, PC-compatible, Closed-loop Laser Positioning Design Your System for Peak Performance The wide variety of optics and laser heads from Agilent gives you maximum design flexibility to achieve your performance goals. In addition to a full range of conventional optics, multiaxis optics provide new possibilities for extremely accurate positioning system designs. Several laser heads offer different sizes and axis velocities to meet your requirements. Remote receivers with fiber-optic pickups allow maximum layout flexibility while removing electronics heat from the measurement area for superior repeatability. Optical wavelength tracking also assists you in achieving unsurpassed measurement repeatability. This product overview covers laser head specifications. Then, the major part of the product overview is devoted to the many optics Agilent has developed for directing the laser beam and making a wide variety of measurements. Accessories and receivers are covered next. Finally, an extensive configuration guide illustrates a number of optical layouts for specific applications. These examples are provided to help you design an optical layout that meets your measurement needs. Configuring Your System All laser-interferometer positioning systems use a laser head, optics, and electronics. After investigating the choices in this product overview and its companion electronics data sheets, you can configure your system by: 1. First choosing a backplane based on the other system electronics you want to use or the outputs you need, 2. then choosing a laser head based on size and velocity requirements, 3. selecting the optics that best match your application needs, and 4. finally, selecting the environmental compensation that meets your accuracy needs. Laser Head Optics * Directing * Measuremen t Measurement Receivers Object Und Control er Power Supply * Powe r * Drive Amplifier M * Servo otor -Lo Compe op nsation Compen sation Measur ement Electr onics Enviro Sensonmental rs Host Comp uter 3 Laser Head Specifications Four laser heads are available for different size, velocity, and interface requirements. The Agilent 5517 series of laser heads provides choices for all available size and velocity requirements in a consistent interface. The 5517A is the basic laser head. The 5517B offers 25% greater axis velocity in a smaller package. The 5517C offers still higher velocity, 75% higher than the 5517A. The 5517D offers the highest axis velocity and is the same size as the 5517B. Standard beam diameter is 6 mm. In addition, there are two beam size options available for the 5517C. Option 003 provides a 3-mm beam diameter for use with the Agilent 10719A and 10721A differential interferometers and 10737L/R compact three-axis interferometers. Option 009 provides a 9-mm beam diameter for use with the 10735A and 10736A three-axis interferometers. The larger beam allows these interferometers a larger angular range of measurement. Finally, the Agilent 5501B laser head is available to replace the previous 5501A laser head in existing applications that require the same polarization, cabling, and electrical power as the 5501A. The 5501B also offers improved accuracy, reliability, and serviceability compared to the previous 5501A. All laser heads use a proven long-life laser tube with a demonstrated Mean Time Between Failure greater than 50,000 hours of operation, making them the most reliable lasers of their type available. 4 Agilent 5501B and 5517A/B/C/D Laser Heads Physical Characteristics Weight: 5517A: 5.5 kg (12 lb) 5517B/C/D: 3.4 kg (7.5 lb) 5501B: 3.4 kg (7.5 lb) Warm-Up Time: less than 10 minutes (5 minutes typical) Magnetic Field Strength (Non-Operating): Does not exceed 5.25 milli-Gauss at a distance of 4.6 m (15 ft) from any point on the surface of the packaged Laser Head. Clearance required for cabling: 5517A: 12.0 cm (4.72 in) beyond back of unit 5517B/C/D: 10.16 cm (4.0 in) beyond back of unit 5501B: 7.5 cm (3.0 in) beyond back of unit Power Power Requirements: (5517A) +15V 0.3V at 2.5A max -15V 0.3V at 0.02A max (5517B/C/D) +15V 0.3V at 2.2A max -15V 0.3V at 0.02A max (5501B) +15V 0.3V at 0.79A max -15V 0.3V at 0.67A max Power Dissipation (nominal): Warm-Up: 35W (5517A/B/C/D) Operation: 23W (5517A/B/C/D) Maximum: 21.9W (5501B) Laser Characteristics Type: Helium-Neon, Continuous Wave, Two-Frequency Minimum Beam Power Output: 180 W Maximum Beam Power Output: 1 mW Std. Beam Diameter: 6 mm (0.25 in) typical 5517C Opt 003:3 mm (0.125 in) 5517C Opt 009:9 mm (0.375 in) Vacuum Wavelength Accuracy (3 , lifetime): 0.1 ppm (0.02 ppm with factory calibration to MIL-STD 45662) Nominal Vacuum Wavelength: 632.991372 nm (5501B, 5517A/B) 632.991354 nm (5517C/D) Vacuum Wavelength Stability (one hour): 0.002 ppm typical Vacuum Wavelength Stability (lifetime): 0.02 ppm typical Safety Classification: Class 2 Laser Product conforming to U.S. National Center for Devices and Radiological Health Regulations 21 CFR 1040.10 and 1040.11. Reference Frequency: 5517A: 1.5-2.0 MHz 5517B: 1.9-2.4 MHz 5517C: 2.4-3.0 MHz 5517D: 3.4-4.0 MHz 5501B: 1.5-2.0 MHz 83.7 mm (3.30) M8 X 1.25 THREAD (3 PLACES) 167.5 mm (6.59) 142.0 mm (5.59) 360.0 mm (14.17) 13.0 mm (0.51) 458.0 mm (18.03) 479.0 mm (18.85) 120.0 mm MIN CLEAR (4.72) 25.0 mm (0.98) 83.7 mm (3.30) 118.0 mm (4.65) 6 mm (0.24) DIA BEAM 435.0 mm (17.13) 83.0 mm (3.27) 192.0 mm (7.56) 22.3 mm DIA (0.88) BEAM 55.1 mm (2.17) 118.0 mm (4.65) 49.5 mm (1.95) Agilent 5517A 13.7 (0.54) 7.11 (0.28) FULL RADIUS 25.4 MAX (1.00) Agilent 5501B Rear Panel 34.6 (1.36) 128.3 (5.05) 34.6 (1.36) 128.3 (5.05) DETAIL 3 PLACES 139.6 (5.50) 208.3 (8.20) 132.0 (5.20) CL 53.3 (2.30 in) 17.7 (0.70) 3.2 (0.13 DIA L.E.D. 8 PLACES 19.3 (0.76) 101.6 (4.0) 325.2 1 (12.80 0.04) 106.4 (4.19) 6 (0.24) DIA BEAM 43.4 DIA (1.71) 70.1 (2.76) 68.0 (2.68) 11.43 (0.45) 20.2 (.80 in) 45.6 (1.80 in) 17.7 (0.70) 10.7 (0.42) 6.55 (0.26) BEAM 79.5 1.0 (3.13 0.04) 128.3 (5.05) CL 3.2 (0.13) DIA L.E.D. 8 PLACES 19.3 (0.76) 70.1 (2.76) 78.6 (3.1) Agilent 5517B/C/D Rear Panel 358.6 (14.12) Agilent 5501B, 5517B, 5517C, 5517D Note: Dimensions of all drawings in this product overview are given in millimeters, with corresponding dimensions in inches given in parentheses. CAUTION LASER LIGHT DO NOT STARE INTO BEAM MAXIMUM OUTPUT 1mw PULSE SPEC continuous wave LASER MEDIUM helium neon CLASS II LASER PRODUCT 5 Directing Optics Specifications A variety of beam splitting and directing optics allows maximum flexibility in optical layouts. Unless otherwise noted, all optics are designed for beam diameters of 6 mm or less. These optics all have housings for standard mounting techniques. Beams of 9-mm diameter can be used with the Agilent 10735A/10736A to provide greater angular range. For directing 9-mm beams, the 10725A, 10726A, and 10728A must be used. These are bare optics that require user-supplied mounts. 10700A 33% Beam Splitter Use: Reflects 1/3 of the total incoming laser beam, transmits 2/3 Weight: 62 g (2.2 oz) 10701A 50% Beam Splitter 0.8 mm (0.03) OFFSET 19.6 mm (0.77 TYP) Use: Reflects 1/2 of the total incoming laser beam, transmits 1/2 Weight: 62 g (2.2 oz) #6-32 UNC (2 PLC'S) THRU CLEARANCE FOR #4 OR 2.5 mm 10707A Beam Bender Use: Bends incoming beam at a 90 angle Weight: 58 g (2.1 oz) 10.16 mm APERTURE (0.40 DIA) CL CL 25.4 mm (1.0) 19.6 mm (0.77) 25.4 mm (1.0) 6 19.6 mm (0.77) #4-40 (0.15 DEEP) (2 SIDES) 25.4 mm (1.0) 19.6 mm (0.77) 25.4 mm (1.0) 10567A Dual Beam Beam Splitter 4 HOLES 8/32 UNC ALL FACES Use: 50% beam splitter which allows both of the split beams to return through the splitter parallel to the incoming beam. Useful when it is necessary to minimize the number of optical ports (for example in a vacuum chamber), or when both receivers must be mounted in the same area. Weight: 317 g (11.3 oz) RETURN TYP 35.6 mm (1.40) EXIT 19.1 mm (0.75) RETURN 53.3 mm (2.10) 12.7 mm (0.50) 12.7 mm (0.50) 12.7 mm (0.50) 21.6 mm (0.85) ENTRANCE RETURN EXIT 12.7 mm (0.50) RETURN 19.1 mm (0.75) 50.8 mm (2.00) 2.41 0.25 10725A 9-mm Laser Beam Splitter Use: 50% beam splitter; divides the beam into equal parts, transmits one part straight through and bends the other part at a 90 degree angle. It is designed for use with beams of 9-mm diameter and smaller. This bare optic requires a user-supplied mount. Weight: 2 g (0.07 oz) 019.3 0.13 10726A 9-mm Laser Beam Bender Use: Bends incoming beam at a 90 degree angle. Like the 10725A, it is designed for use with beams of 9-mm diameter and smaller and is a bare optic that requires a user-supplied mount. Weight: 10 g (0.35 oz) 30.48 45 1 5.59 22 7.62 1 Minimum clear aperture: central 10.05 x 26.92 mm ellipse 10728A 9-mm Laser Beam Plane Mirror Use: Normal incidence plane mirror. Like the 10725A, it is designed for use with beams of 9-mm diameter and smaller and is a bare optic that requires a usersupplied mount. Weight: 21 g (0.74 oz) 34 34 38 4x R 4 38 6.35 Minimum clear aperture: central 34 x 34 mm 7 Measurement Optics Specifications A variety of optics allows maximum measurement flexibility. Unless otherwise noted, all optics are designed for beam diameters of 6 mm or less. The Agilent 10702A Linear Interferometer is the basic interferometer for linear measurements, while the small 10705A Single-beam Interferometer is designed for use in confined spaces. For multiaxis stages, plane mirror interferometers such as the Agilent 10706B are commonly used (see pages 10 and 11). The 10716A high-resolution plane-mirror interferometer provides twice the resolution of the 10706B for the most precise applications (see page 13). The 10715A is a plane-mirror interferometer designed for differential measurements (see page 12). The 10724A Plane Mirror Reflector may be used with these plane mirror interferometers for single-axis measurements (see page 11). directly to the optics column. The Agilent 10735A and 10736A threeaxis interferometers make three measurements simultaneously (linear, yaw, and pitch or roll) for precise wafer positioning in IC-fabrication equipment and other precision stage applications. See pages 14 through 21 for details on these optics. The Agilent 10719A one-axis and 10721A two-axis differential interferometers are designed to optimize the accuracy and repeatability of IC-fabrication equipment by referencing the position of the wafer stage The Agilent 10717A Wavelength Tracker monitors changes in the index of refraction of air to optically compensate for environmental changes (see page 22). Linear Optics BEAM SPACING 10702A Linear Interferometer Use: For general-purpose, single-axis measurements. If the interferometer is the moving component, then 10702A Opt. 001 Windows MUST be ordered, and the interferometer cannot be used to bend the beam. Weight: 10702A: 232 g (8.2 oz) 10702A Opt. 001: 246 g (8.7 oz) 12.7 mm (0.50) CL 28.5 mm (1.12 DIA) #4-40 SCREWS (2) #6-32 UNC (4 PLC'S) THRU CLEARANCE FOR #4 OR 2.5 mm 62.0 mm (2.44) 38.2 mm (1.50) 20.83 mm APERTURE (0.82 DIA) CL 38.2 mm (1.50) 32 mm (1.26 TYP) 33.3 mm (1.31) (4 SIDES) #4-40 x 0.25 DEEP 8 10703A Reflector 20.3 mm APERTURE (0.80 DIA) Use: Paired with 10702A (or 10702A Opt. 001) Linear Interferometer. Cube corner reflector simplifies alignment. If mass is extremely critical, this component is available without housing (10713B). Weight of the bare cube corner is 11.4 g (0.4 oz). Weight: 42 g (1.5 oz) 3 mm (0.12) 33.3 mm (1.31) 37.6 mm (1.48 DIA) 28.4 mm (1.12 DIA) 2.5 mm (0.10) 23.9 mm (0.94) Single Beam Optics 19.5 mm (0.77) BOLT CIRCLE 10704A Reflector Use: Paired with the 10705A Single Beam Interferometer. Cube corner reflector simplifies alignment. If mass is extremely critical, this component is available without housing (10713C). Weight of the bare cube corner is 1.4 g (0.05 oz). Weight: 10.5 g (0.4 oz) 10.2 mm APERTURE (0.40 DIA) 2.5 mm (0.10) 20.5 mm (0.81 DIA) 15.2 mm (0.60) 2.5 mm (0.10) 14.3 mm (0.56) 10705A Single Beam Interferometer #2-56 SCREWS (2) Use: Low mass/limited space single-axis measurements such as disk-drive applications. Can be used to bend the beam, but cannot be used as the moving component. Weight: 85.5 g (3 oz) CL 15.2 mm DIA (0.60) 39.6 mm (1.56) 25.4 mm (1.00) 8.9 mm APERTURE (0.35) 19.5 mm (0.77) CL 25.4 mm (1.00) 19.5 mm (0.77) 19.6 mm (0.77 TYP) #6-32 UNC (4 PLC's) THRU CLEARANCE FOR #4 OR 2.5 mm #2-56 (4 PLACES) 9 Measurement Optics Specifications, continued Plane Mirror Optics 10706B High-Stability Plane Mirror Interferometer Use: Multiple axis applications such as X-Y stage. Can be used to bend the beam, but cannot be used as the moving component. This thermally stable optic is an exact functional replacement for the 10706A Plane Mirror Interferometer. The 10706B design improves measurement stability during temperature changes that affect the optics by reducing measurement drift to 1/12 the value typically achieved by conventional planemirror interferometers such as the 10706A. Weight: 323 g (11.4 oz) Thermal Drift Coefficient (Change of indicated distance per C temperature change): 0.04 m/C (1.6 in/C) typical. Other specifications same as 10706A. 12.7 mm (0.50) 28.4 mm (1.12 DIA) 20.8 mm APERTURE (0.82 DIA) CL 38.1 mm (1.50) 32 mm (1.26 TYP) 38.1 mm (1.50) 33.3 mm (1.31) 38.2 mm (1.50) 10 #4-40 SCREWS (2) BEAM SPACING Typical Measurement Mirror Alignment Requirements for 10706A and B (as a function of distance): 152 mm (6 in): 6 arc-min from normal 305 mm (12 in): 3 arc-min from normal 508 mm (20 in): 1.5 arc-min from normal 4-40 0.25 DEEP (4 SIDES) 14 mm (0.55) 28.5 mm (1.12 DIA) #6-32 UNC (4 PLC'S) THRU CLEARANCE FOR #4 OR 2.5 mm 85.9 mm (3.38) DRIFT AND TEMPERATURE vs. TIME +1.75 27.00 INTERFEROMETER TEMPERATURE MEASUREMENT DRIFT (Microns) +1.50 26.50 +1.25 26.00 CONVENTIONAL PLANE-MIRROR INTERFEROMETER +1.00 25.50 +.75 25.00 +.50 24.50 +.25 24.00 TEMPERATURE (C) Interferometer Thermal Drift This plot shows the measurement drift during optics temperature changes for a conventional plane-mirror interferometer compared with the 10706B High Stability Plane Mirror Interferometer, the 10715A Differential Interferometer, and the 10716A High Resolution Interferometer. The 10706B is nearly as stable as the more expensive 10715A and far more stable than the conventional plane-mirror interferometer. The 10716A has the same stability as the 10706B with two times better resolution. For example, with 0.5C temperature control, measurement drift with the 10706B and 10716A is typically 0.02 microns (0.8 in) compared with 0.25 microns (10 in) with a conventional plane-mirror interferometer. 10715A +0.00 23.50 10706B & 10716A -.25 23.00 0 2.4 4.8 7.2 9.6 12 14.4 16.8 19.2 21.6 24 TIME (Hrs.) INTERFEROMETER TEMPERATURE MEASUREMENT DRIFT 10724A Plane Mirror Reflector Use: This reflector may be used with the 10706A and B, 10715A, and 10716A interferometers for single-axis measurements. Weight: 50 g (1.8 oz) Adjustment Range: 1 (Alignment hardware included) Reflectance: 98% at normal incidence 20.066 mm (0.790) Recommended Plane Mirror Specifications (for 10706A and B, 10715A, and 10716A reflectors) Reflectance: 98% at 633 nm at normal incidence Flatness: Flatness deviations will appear as measurement errors when the mirror is scanned perpendicular to the beam. Recommended range is /4 (0.16 m or 6 in) to /20 (0.03 m or 1.2 in) dependent on accuracy requirements. Optical Surface Quality: 60-40 per Mil 0-13830 2X o 3.556 mm (0.140) THRU 3.810 mm (0.150) 42.164 mm (1.660 DIA) 28.388 mm (1.118 DIA) o 36.068 mm (1.420) 3X 2-56 NC-CLASS 3 THRU 120APART o 32.766 mm (1.290) o 22.860 mm (0.900) APERTURE 11 Measurement Optics Specifications, continued Differential Interferometer 10715A Differential Interferometer Use: Performs differential measurements between the supplied reference mirror and a measurement plane mirror. Provides the best long-term stability of any plane mirror interferometer in plane mirror applications. Minimizes deadpath. The Agilent 10715A eliminates thermal drift in measurements because the entire optical path through the interferometer is common mode. Alignment is slightly more complex than the 10706A/B. For optical layouts requiring the interferometer to turn the beam, the 10715A Opt. 001 must be used. Weight: Interferometer: 594 g (1.31 lb) Reference Mirror: 3.2 g (0.1 oz) 8.1 mm 2 X R 3.2 mm 2 X R 3.6 mm Typical Measurement and Reference Mirror Alignment Requirements (as a function of distance): 2.5 arc-min for 152 mm (6 in) 1.3 arc-min for 305 mm (12 in) 0.7 arc-min for 508 mm (20 in) 6.3 mm EITHER BOTH REFERENCE OR MEASUREMENT BEAMS 12.7 mm 22.9 mm 5.1 mm 5723' For complete dimensions see drawing on next page. 3.4 mm 5.1 mm 9.9 mm EITHER BOTH REFERENCE OR MEASUREMENT BEAMS 18.3 mm PART NUMBER: 10715-20205 WEIGHT: 3.2 GRAMS Reference Mirror for Agilent 10715A 12 10716A High Resolution Interferometer Use: Single and multiple axis high resolution applications such as precision X-Y stages. The Agilent 10716A High Resolution Interferometer improves the system measurement accuracy and repeatability by providing two times better measurement resolution along with the same thermal stability as the 10706B. For optical layouts requiring the interferometer to turn the beam, the 10716A Opt. 001 must be used. Weight: 502 g (1.11 lb) Thermal Drift Coefficient (Change of indicated distance per C temperature change): 0.04 m/C (1.6 in/C) typical 12.7 mm (0.50) SYM @ CL Typical Measurement Mirror Alignment Requirements: Depends on the distance between the interferometer and plane mirror. Typical mirror pitch/yaw angles are: 6 arc-min for 152 mm (6 in) 3 arc-min for 305 mm (12 in) 2 arc-min for 508 mm (20 in) 38.9 mm (1.53) A 90.2 mm* (3.55) 12.7 mm (0.50) 85.9 mm (3.38) B 32.0 mm (1.26) 8.1 mm (0.32) 23.9 mm (0.94) 28.4 mm (1.12) 6-32 UNC (4 PLC'S) THRU CLEARANCE FOR #4 OR 2.5 mm 32.0 mm (1.26) 38.1 mm (1.50) 12.7 mm (0.50) TO MIRRORS FROM LASER TO RECEIVER 28.4 mm (1.12) *FOR 10715A OPTION 001 and 10716A Option 001 THIS DIMENSION IS 100.1 mm (3.94) 14.0 mm (0.55) Agilent 10715A and 10716A 13 Measurement Optics Specifications, continued Multiaxis Optics Improve Positioning Accuracy for Sub-0.5micron Lithography and Other Applications Agilent offers three styles of multiaxis interferometers that make linear and angular measurements. This gives you greater control of multiaxis stages and allows better overall system accuracy. Each style is available in two models. These six interferometers provide linear and angular measurements for up to five degrees of stage freedom (X, Y, pitch, roll, and yaw). This gives you the capability to measure and position an object with higher precision than linear measurements alone. Finer linewidths in ICs and more accurate parts can result from the additional angular measurement and control available with these interferometers. Increase system accuracy and reduce costs * Maximize system accuracy. Multiaxis optics provide measurement and control of stage rotations for improved overlay accuracy. * Lower installation costs. Referenced optics, kinematic installation, prealigned fiber-optic receiver mounts, and no interaxis adjustments make installation easy. * Maximize thermal stability. Monolithic optics and equal glass path lengths minimize errors due to thermal drift. * Lower manufacturing costs. Multiaxis optics reduce the number of components to install. * Maximize mechanical stability. Monolithic optics provide tight interaxis coupling and minimize errors due to vibration. * Lower service cost. Fiber-optic receivers are mounted in a convenient location, and Agilent multiaxis interferometers are easy to remove or install. * Minimize error due to interaxis misalignment. Optical design provides guaranteed interaxis parallelism, no longer dependent on installation. The Agilent 10719A and 10721A perform one- and two-axis differential measurements respectively. Differential measurements provide highly accurate position information using an object such as an optical column as a position reference. This reduces system errors in those applications. The Agilent 10737R, 10737L, 10735A, and 10736A each perform three measurements, one linear and two angular. These three measurement paths have built-in interaxis alignment to give high system accuracy. The 10737R and 10737L use a 3-mm laser beam for a compact optic package. The 10735A and 10736A can use a 9-mm laser beam to provide the widest angle range available. Agilent 10719A and 10721A Agilent 10735A and 10736A Option 001 14 Applications * Lithography * Precision machining * Advanced metrology * R & D on multiaxis stage control * Stage travel characterization * Stage or tool alignment Multiaxis measurements allow smaller linewidths, wider fields, and higher throughputs Small linewidths and stage motion errors due to imperfect ways generally require state-of-the-art wafer steppers to control rotational misalignment about the Z axis (Yaw). This has typically been done with two discrete interferometers that require careful alignment during installation. Agilent now offers multiaxis interferometers that make linear and rotational measurements in a single compact package, conserving valuable space. The interferometers were designed for excellent built-in parallelism, providing an interaxis alignment superior to a careful alignment of discrete interferometers. This helps improve the grid accuracy needed for smaller linewidths. Agilent multiaxis interferometers can measure the pitch and roll of the multiaxis stage due to leveling and stage movement errors, making it possible to calculate and compensate for the change in Abbe error. The quick correction saves the time of performing a site-by-site alignment, thus improving throughput. Mirror mapping improves multiaxis stage performance The yaw of a multiaxis stage is measured using a two- or three-axis interferometer located on either the X or Y axis. When yaw is measured redundantly (on both the X and Y axes), the system has the additional capability of mirror mapping. Mirror mapping allows you to measure and compensate the flatness deviations in the stage mirrors. This improves total system accuracy. L P RO L YAW Internal optics are referenced to their housings, allowing the interferometers to be kinematically located, then bolted into a precision mount without adjustment. Built-in parallelism and referenced optics save the manufacture and service time due to difficult multiaxis alignments. These features also help achieve better overlay accuracy than typically possible with discrete interferometers. Pitch and roll measurements enhance wide field optical lithography To reduce linewidths, optical lithography systems such as i-line and deep UV are moving toward larger numerical apertures. The shallower depth of field resulting from a larger numerical aperture can require site-by-site wafer leveling about the X and Y axis (pitch and roll) to achieve focus over a wide field. Unfortunately, X-Y alignment accuracy suffers because the Abbe error, neutralized during the global alignment, changes during wafer leveling. IT C H Multiaxis interferometric measurements of stage angles enhance the accuracy and throughput of fine-line, wide-field lithography systems. 15 Measurement Optics Specifications, continued The 10719A and 10721A allow columnreferenced measurements The Agilent 10719A and 10721A One-axis and Two-axis Differential Interferometers measure the linear distance between two objects, instead of the distance between the interferometer and an object. This offers a high degree of immunity to unwanted interferometer displacement such as the thermal expansion between the optical column and the interferometer. Errors common to the reference and measurement path are removed because both are equally affected. This improves overlay accuracy in some lithography systems. The Abbe offset error is also decreased by using a small 3-mm beam. Both interferometers are modular and compact, making it easier to build customized measurement systems with one to six axes. The 10719A makes either a differential linear or angular measurement. The linear measurement gauges the displacement between two objects such as an optical column and a stage. Alternatively, the 10719A measures either pitch or roll. Column referencing enhances semiconductor inspection Mask and IC inspection typically require the stage to be moved linearly by small increments with respect to an inspection instrument such as a microscope. This is required in order to compare a desired image with the newly created image. The 10719A was designed to make linear measurements referencing an object such as an inspection tool. Additional features that increase accuracy and decrease cost * Monolithic optics * Guaranteed interaxis parallelism * Prealigned fiber-optic remote receiver mounting * Referenced optics * Kinematic Installation X-ray systems benefit from column referencing X-rays provide finer linewidth lithography because the wavelengths are shorter than optical wavelengths. Slight yaw misalignment reduces the capability even more in these systems than optical lithography systems, because of the finer linewidths. A method to achieve the required accuracy is to reference the multiaxis stage movement to the mask holder. The 10719A and 10721A have been optimized to perform these measurements. Improve overlay accuracy with the Agilent 10719A/10721A by referencing the imagemaking column. The 10721A simultaneously performs two differential measurements, linear and angular (yaw) displacement. Both measurements reference an external mirror mounted to an object such as a column. Column Reference Mirror Wafer Ref. Beam Meas. Beam Stage 16 Measurement Mirror 10719A or 10721A 10719A One-axis Differential Interferometer 10721A Two-axis Differential Interferometer 10719A/10721A Installation Requirements/Recommendations Use: Single- and multiple-axis applications where the stage must be linearly positioned with respect to an external object such as a column or inspection tool. Alternatively, an angle is measured when both reference and measurement beams measure to the same mirror. Specifications Weight: 300 g (11 oz) Axes: Linear, pitch, or roll Available Beam Size: 3 mm Thermal Drift Coefficient (Average): 150 nm (5.9 in) /C Resolution* Linear: 0.6 nm Pitch/roll: 0.03 rad (0.007 arc-sec) Angular Range** (at 300 mm): Pitch/roll: 0.44 mrad (1.5 arc-min) Parallelism (Input to output beams): <0.1 mrad (20 arc-sec) Use: Multiaxis applications where the stage must be positioned linearly and angularly with respect to an external object such as a column or inspection tool. Specifications Weight: 300 g (11 oz) Axes: Linear and yaw Available Beam Size: 3 mm Thermal Drift Coefficient (Average): 150 nm (5.9 in) /C Resolution* Linear: 0.6 nm Yaw: 0.05 rad (0.01 arc-sec) Angular Range** (at 300 mm): Yaw: 0.44 mrad (1.5 arc-min) Parallelism (Input to output beams): <0.1 mrad (20 arc-sec) Installation and Alignment: Kinematic installation requires a referenced surface. See "Laser and Optics Users Manual" for complete installation procedure. Interaxis Alignment: All internal optics are referenced to mounting surface and prealigned. Receivers: Agilent 10780F fiber optic remote receivers. Receiver Alignment: Self aligning when mounted to interferometer. Measurement and Reference (Plane) Mirror Recommendations: Same as 10706A/B; see page 11. 12.70 mm (0.500) NOTE: Flatness deviations will appear as measurement errors when the mirror is translated across the beam. The mirror mount should not bend the mirror. If accuracy requirements demand it, mirror flatness may be calibrated (scanned and stored in the system controller) to be used as a correction factor. 12.70 mm (0.500) Two beams to reference mirror Output Aperture (or Input) Two beams to measurement mirror 31.75 mm (1.250) Input Aperture for 3 mm input beam 10719A Rear View Front View 3.18 mm (0.125) Fiber Optic sensor head mounting pins 31.75 mm (1.250) Four mounting holes on top and bottom surfaces. (6-32) 31.75 mm (1.250) 28.98 mm (1.141) 19.05 mm (0.750) 9.12 mm (0.359) NOTE: Dimensions given in millimeters and (inches) 38.10 mm (1.500) 9.53 mm (0.375) 19.86 mm (0.782) 7.16 mm (0.282) 9.12 mm (0.359) 57.15 mm (2.250) 7.16 mm (0.282) Four beams to reference mirror Ref 60.33 mm (2.375) 19.05 mm (0.750) These specifications are for the 10897B electronics. Four beams to measurement mirror Meas 31.75 mm (1.250) 31.75 mm (1.250) 10721A Output Aperture #1 Input Aperture for 3 mm input beam 12.70 mm (0.500) spacing between linear measurements Output Aperture #2 10719A * Resolution is dependent on the electronics used. ** Angular range is the maximum measurement mirror angle due to all components (i.e., yaw and pitch or yaw and roll) between the measurement mirror and the interferometer for a 6-axis system. Angular range is dependent on the measurement distance. Angular range is reduced when the reference mirror is misaligned. 12.70 mm (0.500) 10719A/10721A 10721A 17 Measurement Optics Specifications, continued 10737L and 10737R Compact Three-Axis Interferometers Improve positioning accuracy of precision equipment with lowercost, multiaxis laser measurements. Multiaxis measurements improve accuracy by providing greater control of multiaxis stages. Each linear and angular degree of freedom can be measured and controlled to compensate for mechanical imperfections in the stage's motion. The new Agilent 10737L and 10737R Compact Threeaxis Interferometers provide this capability in a more compact, lowercost package than the 10735A and 10736A Three-axis Interferometers. This allows higher accuracy from multiaxis measurements to be achieved in smaller, lower-cost equipment than was previously possible. Each 10737L and 10737R makes three linear measurements. Two angular measurements can be calculated from this data. Two of these interferometers used together provide redundant yaw measurements, which allow mirror mapping. Mirror mapping improves accuracy by compensating for mirror flatness deviations. The 10737L and 10737R also reduce installation time and cost. All three axes are aligned simultaneously in a process similar to alignment of the 10706B High Stability Plane Mirror Interferometer. Both interferometers include built-in remote pickups for 10780F Option 001 Remote Receivers, which simplifies installation and alignment. A simple snap connection for the fiber optic cable quickly connects the receiver to the remote pickups. Specifications 10737L & 10737R Specifications Comparison to 10735A & 10736A Linear Resolution 5 nm* 0.6 nm** 5 nm* 0.6 nm** Yaw Resolution 0.35 rad (0.07 arc-sec)* 0.04 rad (0.01 arc-sec)** 0.2 rad (0.04 arc-sec)* 0.025 rad (0.005 arc-sec)** Pitch & Roll Resolution 0.7 rad (0.14 arc-sec)* 0.1 rad (0.02 arc-sec)** 0.24 rad (0.05 arc-sec)* 0.03 rad (0.006 arc-sec)** Yaw Range 0.44 mrad (1.5 arc-min) 1 mrad (3.4 arc-min) 1.5 mrad (5.1 arc-min) Pitch & Roll Range 0.44 mrad (1.5 arc-min) 1 mrad (3.4 arc-min) * Using 5527A/B, 10885A, 10895A electronics. ** Using 108978 electronics. 18 The 10737L and 10737R differ only in measurement beam direction; the 10737L turns the beam to the left and the 10737R turns the beam to the right. Both interferometers use the 3-mm beam diameter from the Agilent 5517C Option 003 Laser Head. Using 6-mm beam diameter. Using 9-mm beam diameter. At a distance of 300 mm, maximum measurement mirror angle due to all components (i.e., yaw and pitch or yaw and roll) between the measurement mirror and the interferometer. A six-axis system is assumed. Improve positioning accuracy with more compact, lower-cost multiaxis measurements with the 10737L and 10737R compact three-axis interferometers. Linear Range: 10 m (33 ft) total for all three axes Operating Temperature: 0-40C (17-23C to ensure system non-linearity specification) Thermal Drift Coefficient: 0.1 m/C (40 in/C) typical average for each axis Weight: 490 g (18 oz) Measurement (Plane) Mirror Recommendations Materials Used: Housing: stainless steel and aluminum Optics: optical grade glass Adhesives: vacuum grade Receiver inserts: urethane foam, acetal, 15% glass fill polyester Installation: Uses 3-mm beam available from 5517C Option 003. Requires three 10780F Option 001 Remote Receivers. Compatible with the 10710A Mount. Reflectance: 98% at 633 nm at normal incidence. Flatness: Flatness deviations will appear as measurement errors when the mirror is scanned perpendicular to the beam. Recommended range /4 (0.16 m or 6 in) to /20 (0.03 m or 1.2 in) dependent on accuracy requirements. Optical Surface Quality: 60-40 per Mil 0-13830. Dimensions TOP VIEW 32 mm (1.26) 3x Fiber-Optic Connectors for 10780F Option 001 Receivers 32 mm (1.26) From Laser 4x drilled for clearance of 4-40 screw and tapped 6-32 UNC-2B X .250 deep 4X this side and 4x far side 60.1 mm (2.37) 3.0 mm (0.12) To Plane Mirror 119 mm (4.69) 64.1mm (2.53) 7.19 mm (0.283) Input Apeture. 38.2 mm (1.50) 7.19 mm (0.283) 7.19 mm (0.283) 7.19 mm (0.283) 76.11 mm (3.00) 17.3 mm (0.68) 22.63 mm (0.891) 17.3 mm (0.68) The Agilent 10737L. The dimensions of the 10737R are identical. 19 Measurement Optics Specifications, continued Additional features that increase accuracy and decrease cost * Wide angle range * Monolithic optics * Guaranteed interaxis parallelism * Prealigned fiber-optic remote receiver mounting * Referenced optics * Kinematic Installation The 10735A and 10736A are three-axis optical benches in single packages The 10735A and 10736A Three-axis Interferometers put the functionality of an optical bench with multiple beam benders, beam splitters, and three interferometers in a single highperformance package. This eliminates expensive, time-consuming interaxis setup and alignment. The interferometers split an incoming laser beam into three beams to measure linear distance, pitch, and yaw; or linear distance, roll, and yaw. Custom Agilent factory fixtures and measuring equipment align and lock the parallel beams to guaranteed specifications for greater stability and accuracy than is practical with discrete components. This gives you greater overall system performance. The Agilent 10735A and 10736A replace three interferometers and multiple beam benders and beam splatters with a rigid, high-performance package. 20 Multiaxis installation simplified All axes are referenced to the interferometer's mounting surface for easy kinematic installation onto a usersupplied reference surface. This makes installation as easy as sliding the interferometer into place and bolting it down. The interferometers differ in the beam pattern they produce on the measurement mirror, providing flexibility in system design. Three-axis interferometers provide the highest angular performance available The 10735A and 10736A provide the highest resolution, widest angular range, and most accurately aligned three-axis interferometers available off-the-shelf. The high angular resolution gives you greater control over your multiaxis stage, enabling superior grid accuracy in lithography applications. The wide angular measurement range, with a 9-mm laser beam, allows both global and site-by-site stage correction under interferometric control. This helps to achieve high positioning accuracy without degrading throughput. 10735A/10736A Three-axis Interferometers Use: Multiaxis applications where linear and angular control of the stage is required. The Agilent 10735A and 10736A provide three linear measurements. Two angular measurements can be calculated from this data. When an interferometer is placed along the X axis, yaw (q Z), and pitch (q Y) can be derived in addition to linear (X) displacement. When it is placed on the Y axis, yaw (q Z), and roll (q X) can be derived in addition to linear (Y) displacement. Redundant yaw is useful when mapping measurement mirrors, which provides improved accuracy. The 10735A and 10736A differ in their measurement beam patterns (see drawing). Agilent 10736A Option 001 provides a beam bender for fixed compensation axis. Specifications Weight: 5.5 kg (12 lbs) Axes: 3 linear axes which provide linear (X), pitch, and yaw; or linear (Y), roll, and yaw. Available Beam Diam.: 3/6/9 mm Thermal Drift Coefficient (Average): Axes 1 & 2: 40 nm (1.6 in) /C Axis 3: 100 nm (3.9 in) /C Resolution* Linear: 0.6 nm Yaw: 0.024 rad (0.005 arc-sec) Pitch/roll: 0.03 rad (0.006 arc-sec) Angular Range (at 300 mm displacement)** Pitch/roll: 1 mrad (3.4 arc-min) Yaw (for 6-mm beams): 1 mrad (3.4 arc-min) Yaw (for 9-mm beams): 1.5 mrad (5.1 arc-min) Parallelism (Measurement beams): Axes 1 & 2: <40 rad (8 arc-sec) Axes 1 & 3: <50 rad (11 arc-sec) 203.5 mm (8.01) 179.0 mm (7.05) 10735A/10736A Installation Recommendations Installation and Alignment: Kinematic installation procedure requires three referenced pins mounted onto a referenced surface. See "Laser and Optics Users Manual" for complete installation procedure. Interaxis Alignment: All internal optics are referenced to the mounting surface and prealigned. Receivers: Agilent 10780F Fiber Optic Remote Receivers. Receiver Alignment: Self aligning when mounted to interferometer. Measurement (Plane) Mirror Recommendations: Same as 10706A/B; see page 11. 5.5 mm (0.22) 88.5 mm (3.48) 105.0 mm (4.13) NOTE: Dimensions given in millimeters and (inches) 11.0 mm (0.43) 4X Mounting Holes Input Aperture 10735A 21.0 mm (0.83) 10736A 3 Axis Interferometer 3 Axis Interferometer 31.25 mm (1.23) 10735A 51.3 mm (2.02) 26.0 mm (1.02) 3X 13.11 mm (0.52) 10736A 10735A Axis 3 42.5 mm (1.67) 10736A Axis 3 * Resolution is dependent on the electronics used. 60.0 mm (2.36) Axis 1 Axis 2 Axis 1 Measurement Beam Patterns Axis 2 These specifications are for the Agilent 10897B electronics. ** Angular range is the maximum angle between the measurement mirror and the interferometer for a 6-axis system. Angular range is dependent on the measurement distance. Both angles (pitch and yaw or roll and yaw) can be at the angular limit concurrently. 21 Measurement Optics Specifications, continued Wavelength Tracker 10717A Wavelength Tracker Use: Tracks changes in the air's index of refraction to optically compensate for environmental changes. Weight: 1.7 kg (3.7 lb) Kinematic Mounting: Angular Adjustment Range (at nominal position): Pitch: 1 Yaw: 1 Translation Adjustment Range (at nominal position): Vertical: 3 mm (0.12 in) Horizontal: 3 mm (0.12 in) Mounting Hardware Quantity: 3,10-32 UNF2A Screws Minimum Mounting Clearance Required: 3 mm (0.12 in) around perimeter. Calibration: Not Required. Interface: Measurement receiver, cable, and appropriate electronics required. LASER MOUNTING SURFACE INPUT BEAM FROM LASER OUTPUT BEAM TO RECEIVER 15.88 mm (0.625) 260.35 mm (10.25) 177.80 0.25 mm (7.000 .010) MOUNTING HOLES 3 X 10-32 UNF 2A X 13 (0.5) DP 30.10 0.13 mm (1.185 .005) A B 30.10 0.13 mm (1.185 .005) 32 mm (1.25) 12.70 m (0.500) 67 mm (2.63) 22 CENTERLINE OF LASER BEAM 8.13 mm (0.320) MAX 79.25 mm (3.120) 39.62 mm (1.560) Accessory Specifications Optics mounts can make alignment faster and easier, and are available for most optics. Detailed specifications are below. Optics Mounts 10711A Adjustable Mount 10722A Plane Mirror Converter Use: Mount for Agilent 10702A, 10706A/B, 10715A, and 10716A Weight: 141.1 g (5 oz) Angular Adjustment: Yaw: 5 Tilt: 5 Use: With an additional 10703A, the 10722A can be used to convert a 10702A Linear Interferometer into a 10706A Plane Mirror Interferometer. With an additional 10723A, the 10722A can be used to convert a 10702A into a 10706B. Weight: 35.5 g (1.3 oz) 10710A Adjustable Mount Use: Mount for Agilent 10700A, 10701A, 10705A, and 10707A Weight: 88.2 g (3.2 oz) Angular Adjustment Range: Yaw: 8 Tilt: 8 10723A High Stability Adapter 10711A YAW 32.0 mm (1.26) #4-40 THRU 4 PLC'S 10710A 59.7 mm (2.35) 25.4 mm DIA THRU (1.00) 32.0 mm (1.26) 33.27 mm (1.31) YAW 64.77 mm (2.55) CLEARANCE FOR #4 SCREW (3 mm) #4-40 THRU 4 PLC'S 41.66 mm (1.64) 19.6 mm (0.77) 47.0 mm (1.85) 12.7 mm DIA THRU (0.50) 19.56 mm (0.77) TILT CLEARANCE FOR #4 SCREW (2.5 mm SCREW) 10700A 10701A 10705A 10707A 38.1 mm (1.50) TILT CLEARANCE FOR #4-40 CAP SCREW OPPOSITE SIDE Use: If you already use the 10706A, you can easily convert it to a 10706B with the 10723A High Stability Adapter. With the 10723A you can obtain the much higher thermal stability of the 10706B at nominal cost and effort. Weight: 49 g (1.7 oz) CLEARANCE FOR #4-40 CAP SCREW 2 PLC'S 10702A 10706A/B 10715A 10716A BEAM SPACING 12.7 mm (0.50) 31.75 mm (1.25) 12.7 mm (0.50) 25.4 mm (1.00) BEAM CENTER LINE 25.4 mm (1.00) 12.7 mm (0.50) 27.9 mm (1.10) 23 Receiver Specifications Two different measurement receivers are available to give you design flexibility and maximum system performance. One receiver is required for each measurement axis (including wavelength tracker). The Agilent 10780C affords the highest sensitivity and lowest cost. The 10780F provides slightly less sensitivity, but can improve system performance by enabling you to mount heat-dissipating receiver electronics away from the measurement area. Hence, higher measurement stability and the resulting accuracy and repeatability are obtained. The fiberoptic cable used to attach the remote sensor to the receiver electronics allows design flexibility and easier access to the receiver gain adjustment. LED Beam Diameter 6 mm (0.24) Beam Spacing 54.7 mm (2.15) 24.0 mm (0.945) 1.8 mm (0.070) Gain Adjustment Photodetector Insulating Mounting Pads 38.1 mm (1.50) 107.8 mm (4.25) 11.4 mm (0.45) 76.0 mm (3.0) 2.3 mm (0.09 TYP) Use Only Nylon Mounting Screw 2360-0369 to Avoid Ground Loop Agilent 10780C Receiver 24 12.7 mm (0.50) 7.6 mm (0.30) 15.2 mm (0.60) 114.8 mm (4.52) 9.9 mm (0.39) Clearance hole for M3 (6-32) Screw (2 PLC) 10780C Receiver and 10780F Remote Receiver Specifications Typical Power Requirements: +15 volts at 136 mA Maximum Sensitivity: 1.5 W (10780C) 2.2 W (10780F with 2-m cable) (10780F becomes 5.0 W with a 10-m fiber cable.) Heat Dissipation: 0.0 W for remote sensor 2.0 W typical for receiver Output Signal: Differential square wave at Doppler-shifted split frequency (100 kHz to 7.2 MHz). Fiber-optic Cable Length (10780F): 2 m standard 10 m maximum recommended Alignment Tolerances: Roll: 3 degrees Pitch: 1 degree Yaw: 1 degree (10780F is self aligning when mounted to the 10715A, 10716A, 10717A, 10719A, 10721A, 10735A, and 10736A.) Weight: 136 g (4.8 oz) for 10780C 126 g (4.5 oz) for 10780F 26 g (0.9 oz) for remote sensor with 2-m cable Beam Diameter 6.0 mm (0.24) Beam Spacing 1.8 mm (0.070) LED 54.7 mm (2.15) 24.0 mm (0.945) 7.6 mm (0.30) 12.7 (0.50) 7.6 mm (0.30) 43.1 mm (1.70) 114.8 mm (4.52) 22.4 mm (0.88) 3.5 mm (0.14) 15.5 mm (0.61) Clearance hole for M3 (6-32) Screw (2 PLC) 107.8 mm (4.25) 38.1 mm (1.50) Photodetector 23.8 mm (0.94) 19.1 mm (0.75) 76 mm (3.0) 9.9 mm (0.39) 19.1 mm (0.75) R35 mm Minimum (1.4) Bend Radius 7.6 mm (0.30) Clearance hole for M3 (6-32) Screw (2 PLC) Agilent 10780F Remote Receiver 25 0ptics and Laser Head Configuration Guide Use this configuration guide to design your Agilent laser interferometer positioning system. Generally you will first refer to the appropriate electronics data sheet and choose the electronics accordingly. Then you select your laser head based on size and axis velocity requirements. Next, sketch your optical configuration. From this layout, determine your optics needs. Two additional years of returnto-Agilent service are available at purchase for all laser heads and electronics as Option W30. Contact your local Agilent sales representative for details. Component Needs Comments Laser Head 5517A 5517B 5517C Opt. 003 Opt. 009 5517D 5501B One required per system Laser Head, lowest velocity, largest size Laser Head, 25% more velocity, small size Laser Head, 75% more velocity, small size 3-mm beam diameter for use with 10719A and 10721A 9-mm beam diameter Laser Head, highest velocity, small size Laser Head, lowest velocity, small size, interface same as 5501A Factory Calibration to MIL-STD 45662 is available at extra cost, and may be specified in the order. Directing Optics 10700A 10701A 10707A 10567A 10725A 10726A 10728A Order as required to manipulate beam path to your configuration 33% Beam Splitter 50% Beam Splitter Beam Bender Dual Beam Splitter--useful in vacuum 9-mm Laser Beam Splitter 9-mm Laser Beam Bender 9-mm Laser Beam Plane Mirror Measurement Optics 10702A Opt. 001 10703A 10704A 10705A 10706B 10713B 10713C 10713D 10715A Opt. 001 10716A Opt. 001 10724A 10719A 10721A 10735A 10736A Opt. 001 10737L 10737R 1 interferometer-plus-reflector pair required per axis Linear Interferometer Windows--required if interferometer is the moving component Reflector--paired with 10702A Reflector--paired with 10705A Single Beam Interferometer High Stability Plane Mirror Interferometer One-inch bare cube corner 0.5-inch bare cube corner 0.25-inch bare cube corner Differential Interferometer Turned Configuration High Resolution Interferometer Turned Configuration Plane Mirror Reflector One-axis Differential Interferometer, requires 3-mm beam Two-axis Differential Interferometer, requires 3-mm beam Three-axis Interferometer Three-axis Interferometer Adds beam bender Compact Three-axis Interferometer (Left) Compact Three-axis Interferometer (Right) 26 Measurement Optics Summary 10702A 10705A 10706B 10715A 10716A Application General Purpose Low-mass, Limited Space Plane Mirror High Accuracy Plane Mirror High Resolution Plane Mirror Optics Resolution /2 (316.5 nm) /2 (316.5 nm) /4 (158.25 nm) /4 (158.25 nm) /8 (79 nm) System Resolution* /64 (10 nm) /64 (10 nm) /128 (5 nm) /128 (5 nm) /256 (2.5 nm) Beam Separation 12.7 mm (1/2 in) N/A single beam 12.7 mm (1/2 in) 12.7 mm (1/2 in) 12.7 mm (1/2 in) Reflector 10703A 10704A 10724A 10724A 10724A Reflector Weight 42 g (1.5 oz) 10.5 g (0.4 oz) 50 g (1.8 oz) 50g (1.8 oz) 50g (1.8 oz) Mount Used 10711A 10710A 10711A 10711A 10711A 10717A 10719A 10721A 10735A 10736A Wavelength of Light Compensation One-axis Differential Measurements (Plane Mirror) Two-axis Differential Measurements (Plane Mirror) Three-axis Measurements (distance, pitch, yaw) (Plane Mirror) Three-axis Measurements (distance, pitch, yaw) (Plane Mirror) /4 (158.25 nm) /4 (158.25 nm) /4 (158.25 nm) /4 (158.25 nm) /4 (158.25 nm) /128 (5 nm) /128 (5 nm) 0.26 rad (0.054 arc-sec) /128 (5 nm) 0.4 rad (0.08 arc-sec) N/A /128 (5 nm) 0.24 rad (0.05 arc-sec) 0.2 rad (0.04 arc-sec) /128 (5 nm) 0.24 rad (0.05 arc-sec) 0.2 rad (0.04 arc-sec) Beam Separation N/A see drawing see drawing see drawing see drawing Reflector Integral Custom Custom Custom Custom Reflector Weight N/A Custom Custom Custom Custom Mount Used Integral Custom Custom Custom Custom Application Optics Resolution Linear System Resolution* Linear Pitch Yaw * When used with the Agilent 5527B Laser Positioning Transducer System, 10885A PC Axis Board, or 10895A Laser Axis Board for VMEbus. System resolution is improved by a factor of 2 when using the Agilent 10889B PC Servo Axis Card. The 10897B improves system resolution by a factor of 8. Specifications throughout this document describe warranted performance. Supplemental characteristics (indicated by TYPICAL or AVERAGE) are intended to provide nonwarranted performance information useful in general application. 27 Example Configurations Example 1--Single Axis System for Servo-Track Writing 10704A 10705A 1- 5517B/C Laser Head 1- 10705A Single Beam Interferometer 1- 10704A Reflector (or use bare corner cube) 1- 10780C/F Receiver 1- 10710A Optics Mount 5517A/B 10780C/F Example 2--Multiaxis System for a Coordinate Measuring Machine 1332131463- 5517B Laser Head 10702A Linear Interferometer 10703A Rttroreflector 10700A 33% Beamsplitter 10701A 50% Beamsplitter 10707A Beam Bender 10717A Wavelength Tracker 10780C/F Receiver 10710A Adjustable Mount 10711A Adjustable Mount 10702A 10780C/F 10702A 10707A 10703A 10703A 10701A 10707A 10780C/F 10780C/F 10700A 10717A Z 10707A X Y 10703A 10700A 10780C/F 10707A 10702A 5517B 28 Example 3--Multiaxis System for a Precision X-Y Stage 1- 5517C Laser Head 3- 10701A 50% Beam Splitter 3- 10706B High-Stability Plane Mirror Interferometer 1- 10707A Beam Bender 1- 10717A Wavelength Tracker 4- 10780C/F Remote Receiver 4- 10710A Optics Mount 3- 10711A Optics Mount Yaw 10706B 10706B 10706B X-axis Y-yaw 10780C/F 10701A 10780C/F Y-axis 10780C/F 10701A 10780C/F 10717A 10701A 10707A 5517C Multiaxis System for a Precision X-Y Stage as Used in IC Fabrication 29 Example Configurations, continued Example 4--Three-axis X-Y Stage Laser Positioning System with Column Referencing 1111- 5517C Opt. 003 3-mm Laser Head 10701A 50% Beam Splitter 10707A Beam Splitter 10719A One-axis Differential Interferometer 1- 10721A Two-axis Differential Interferometer 3- 10780F Remote Receiver 3- 10710A Adjustable Mount 5517C Opt. 003 10701A 10707A 10707A Column To 10780F Remote Receivers To 10780F Remote Receiver 10719A 10721A Multiaxis Stage Example 5--Five-axis X-Y Stage Laser Positioning System 11226- 5517C Opt. 009 9-mm Laser Head 10725A 9-mm Laser Beam Splitter 10726A 9-mm Laser Beam Bender 10736A Three-axis Interferometer 10780F Remote Receiver 5517C Opt. 009 10736A 10725A 10726A To Fiber-optic Receivers 30 To Fiber-optic Receivers Multiaxis Stage Agilent Technologies' Test and Measurement Support, Services, and Assistance Agilent Technologies aims to maximize the value you receive, while minimizing your risk and problems. 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