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Laser-Trapped Mirrors in Space 
Elizabeth F. McCormack 
Bryn Mawr College 
Jean-Marc Fournier 
Institute of Imaging and Applied Optics 
Swiss Federal Institute of Technology 
TomaszGrzegorczyk 
Massachusetts Institute of Technology 
Robert Stachik 
Christina River Institute
The Project 
Can Laser Trapped Mirrors be a practical solution to the problemof building large, low-mass, optical systems in Space? 
The Laser-Trapped Mirror (LTM) ConceptNASA Goals 
Light-Induced Trapping Forces 
Role of Optical Binding 
Experimental Work 
Numerical Calculations 
Project Goals
The LTM DesignTRAPPED MIRRORLaserMirrorStar LightCCDParticle sourceMirrorStanding wave of laser light traps particles(Labeyrie, A&A, 1979)(1979)
The LTM Concept 
Beams emitted in opposite directions by a laser strike two deflectors. Reflected light produces a series of parabolicfringe surfaces. 
Through diffractive and scattering forces, dielectric particles are attracted toward bright fringes, and metallic particles towards dark fringes. 
Ramping the laser wavelength permits sweeping 
of particles to the central fringe. 
Result is a reflective surface in the shape of 
a mirror of almost arbitrary size.
Advantages of the LTM 
Potential for very large aperture mirrors 
with very low mass (35 m--> 100g !!) and 
extremely high packing efficiency 
(35m--> 5 cm cube). 
Deployment without large moving parts, 
potential to actively alter the mirror’s shape, and 
flexibility to change mirror “coatings” in orbit. 
Potential for fabricating “naturally” co- phased arrays of arbitrary shape as shown at left. 
Resilience against meteoroid damage (self-healing). 
The LTM should be diffraction limited at long 
wavelengths. For a trapping wavelength in the 
visible, e.g. 0.5 μm, and operation at 20 μm, 
the “flatness” of the mirror will be better than λ/80.
NASA GoalsFuture NASA Optical Systems Goals and their relation to the LTM 
Visible 
Far IR to sub mm 
Proposed work 
Additional comments 
Wavelength / Energy Range 
400 -700 
nm 
20 –800 μm 
Demonstration of 
a mirror at >500 nm and in the near IR 
LTM can also be use as a diffractive structure and can work at different wavelengths in different view directions simultaneously 
Size 
6-10+ m 
10-25 m 
1 cm 
Structures of about 80 microns radius have been made in water. We will extend this work to understand the trapping of much larger numbers of particles where binding forces dominate. 
ArealDensity 
<5 kg/m2 
< 5 kg/m2 
< 10-6kg/m2for the mirror alone and 
< 0.1 kg/m2for the system 
Surface Figure 
λ/150 
at 
λ=500 nm 
λ/14 at 
λ=20 μm 
λ/ 2 confinement at 
λ=500 nm 
(or better, if binding helps to reduce thermal agitation) 
and imaging at 
λ=20 μm 
gives”flatness” 
λ/80 
In the first order, the surface figure of an LTM is independent of the size of the particles used, however, particle size will be an important factor for determining surface quality through reflectivity and scattering cross-sections.
Previous WorkExperiments by Fournier et al. in the early 1990’s demonstrated laser trapping of arrays of macroscopic particles along interference fringes: M. Burns, J. Fournier, and J. A. Golovchenko, Science 249, 749 (1990). Fournier et al. also observed that laser trapped particles can self-organize along a fringe due to photon re-scattering among the trapped particles resulting in "optical matter" (analogous to regular matter, which is self-organized by electronic interactions): M. Burns, J. Fournier, and J. A. Golovchenko, Phys. Rev. Lett. 63, 1233 (1989). λ
The Forces of Light 
Light fields of varying intensity can be used to trap particles. Light reflectionresults in repulsion (scattering force). Light refractionresults in attraction (induced dipole and field gradient forces). Strongly wavelength-dependent processes. scattering forcegradient forcebinding force
Fscat〈Fscat〉= 1/3 α2k4〈E2〉 Fgrad〈Fgrad〉= α. ∇〈E2〉 Trapping in a Gaussian Beam
Trap Strength 
Dipole interaction traps dielectric particles in regions of highfield intensity. U=P⋅E≅12 αE⋅Eα=n2−1n2+1a3 
For two counter-propagating plane waves, the trap strength is: Utrap=2πα cI 
For 1 micron-sized particles with a reasonable index of refraction, n=1.6 
and I expressed in Watts/m2: This is the challenge; this number is very small.Utrap=6×10−20I 
Equivalent to a temperature of milliKelvins 
and an escape velocity of 10-4cm/s. 
Compare to infrared background at T ~ 30K
Estimate of Evaporation Time 
At 30 K, background photons: nγ ∼ 106cm-3, λ= 10-2cm. ΔE= pγ2 2m=(h/λ)22m 
ΔE ~ 10-34ergs/collision 
Given a cross-section, σ = 10−2 σ, for the interaction of silica with 
these photons, the rate of increase of the kinetic energy of a trapped particle is: dEdt=ΔEnγσc 
dE/dt ~ 10-26ergs/sec 
Integrating and evaluating for a 1 micron-sized particle, we get: τevap=4παmλ2h2nγσc2Iτevap≈1.5×108Isec 
where Iis expressed in Watts/m2. 
A respectable number: about 5 yearsfor I = 1 Watt/m2and ~ months for currently available laser intensities. with radius ~a: Particle size is critical. 100 nm-sized particles --τevap~ hours, will need damping.
Consider all fields: Incident and scattered, Near and farPair of oscillators: Driven by fields andradiating like dipolesSolve for self-consistencyOptical Binding Force
Optical Binding Potential 
Induced dipole moments in adjacent spheres will give rise to electromagnetic forces between the spheres. Burns, et al. give an approximation for this interaction energy: long-range interaction which oscillates in sign at λand falls off as 1/r. Calculations of this two-particle binding potential look encouraging. However, results are based on approximations not necessarily valid in theregime where particle radius ~ λ. Need to explore this effect with no approximations, i.e., in theMiescattering regime.
InterferometricTemplates 
2 Beams3 Beams
One-and Two-Dimensional Traps20 20 μμmm20 20 μμmm 
1500 traps2.8 2.8 μμmm2 2 μμmm 
2 Beams 
3 Beams
Observation of optical binding and 
trapping in a Gaussian beam 
1beam 
Auto-arrangement of 3 μm polystyrene beads at the waist of a Gaussian beam
2-Beam Interference 
Voltage supplyfiltersCCDpiezo- electric elementMOsample2 2 μμm beads in motorizedm motorizeddragged celldragged cellFringes translation withFringes withpiezopiezo--electric elementelectric element
Optical Binding in 2-Beam Trap
3-Beam Interferencetemplategeneration 
intensity patternPiezoimagingsystemCCD
Optical Binding in 3-Beam TrapJ.-M. Fournier, M.M. Burns, and J.A. Golovchenko, “Writing Diffractive Structures by Optical Trapping”, Proc. SPIE 2406 “Practical holography”,pp. 101-111, 1995. M.M. Burns, J.-M. Fournier, and J.A. Golovchenko, Optical Matter, US Patent # 5,245,466, 1993
Force Calculation: Single Plane Wave
Force Calculation: Gaussian Beam
Force Calculation: Three Intersecting Plane Waves
Project Goals 
Demonstrate and characterize a small, floating LTM in water. Develop and use computational algorithms to model an LTM which include all optical forces including optical binding effects. Combine lab measurements with particle design and the computational models to obtain estimates for the mirror stability and quality, and for the laser power requirements in a vacuum environment.
Laser Trapped Mirrors in SpaceArtist’s view of Laser Trapped MirrorArtist’s Mirror(NASA study by Boeing(Boeing--SVS)

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1202 mccormack[2]

  • 1. Laser-Trapped Mirrors in Space Elizabeth F. McCormack Bryn Mawr College Jean-Marc Fournier Institute of Imaging and Applied Optics Swiss Federal Institute of Technology TomaszGrzegorczyk Massachusetts Institute of Technology Robert Stachik Christina River Institute
  • 2. The Project Can Laser Trapped Mirrors be a practical solution to the problemof building large, low-mass, optical systems in Space? The Laser-Trapped Mirror (LTM) ConceptNASA Goals Light-Induced Trapping Forces Role of Optical Binding Experimental Work Numerical Calculations Project Goals
  • 3. The LTM DesignTRAPPED MIRRORLaserMirrorStar LightCCDParticle sourceMirrorStanding wave of laser light traps particles(Labeyrie, A&A, 1979)(1979)
  • 4. The LTM Concept Beams emitted in opposite directions by a laser strike two deflectors. Reflected light produces a series of parabolicfringe surfaces. Through diffractive and scattering forces, dielectric particles are attracted toward bright fringes, and metallic particles towards dark fringes. Ramping the laser wavelength permits sweeping of particles to the central fringe. Result is a reflective surface in the shape of a mirror of almost arbitrary size.
  • 5. Advantages of the LTM Potential for very large aperture mirrors with very low mass (35 m--> 100g !!) and extremely high packing efficiency (35m--> 5 cm cube). Deployment without large moving parts, potential to actively alter the mirror’s shape, and flexibility to change mirror “coatings” in orbit. Potential for fabricating “naturally” co- phased arrays of arbitrary shape as shown at left. Resilience against meteoroid damage (self-healing). The LTM should be diffraction limited at long wavelengths. For a trapping wavelength in the visible, e.g. 0.5 μm, and operation at 20 μm, the “flatness” of the mirror will be better than λ/80.
  • 6. NASA GoalsFuture NASA Optical Systems Goals and their relation to the LTM Visible Far IR to sub mm Proposed work Additional comments Wavelength / Energy Range 400 -700 nm 20 –800 μm Demonstration of a mirror at >500 nm and in the near IR LTM can also be use as a diffractive structure and can work at different wavelengths in different view directions simultaneously Size 6-10+ m 10-25 m 1 cm Structures of about 80 microns radius have been made in water. We will extend this work to understand the trapping of much larger numbers of particles where binding forces dominate. ArealDensity <5 kg/m2 < 5 kg/m2 < 10-6kg/m2for the mirror alone and < 0.1 kg/m2for the system Surface Figure λ/150 at λ=500 nm λ/14 at λ=20 μm λ/ 2 confinement at λ=500 nm (or better, if binding helps to reduce thermal agitation) and imaging at λ=20 μm gives”flatness” λ/80 In the first order, the surface figure of an LTM is independent of the size of the particles used, however, particle size will be an important factor for determining surface quality through reflectivity and scattering cross-sections.
  • 7. Previous WorkExperiments by Fournier et al. in the early 1990’s demonstrated laser trapping of arrays of macroscopic particles along interference fringes: M. Burns, J. Fournier, and J. A. Golovchenko, Science 249, 749 (1990). Fournier et al. also observed that laser trapped particles can self-organize along a fringe due to photon re-scattering among the trapped particles resulting in "optical matter" (analogous to regular matter, which is self-organized by electronic interactions): M. Burns, J. Fournier, and J. A. Golovchenko, Phys. Rev. Lett. 63, 1233 (1989). λ
  • 8. The Forces of Light Light fields of varying intensity can be used to trap particles. Light reflectionresults in repulsion (scattering force). Light refractionresults in attraction (induced dipole and field gradient forces). Strongly wavelength-dependent processes. scattering forcegradient forcebinding force
  • 9. Fscat〈Fscat〉= 1/3 α2k4〈E2〉 Fgrad〈Fgrad〉= α. ∇〈E2〉 Trapping in a Gaussian Beam
  • 10. Trap Strength Dipole interaction traps dielectric particles in regions of highfield intensity. U=P⋅E≅12 αE⋅Eα=n2−1n2+1a3 For two counter-propagating plane waves, the trap strength is: Utrap=2πα cI For 1 micron-sized particles with a reasonable index of refraction, n=1.6 and I expressed in Watts/m2: This is the challenge; this number is very small.Utrap=6×10−20I Equivalent to a temperature of milliKelvins and an escape velocity of 10-4cm/s. Compare to infrared background at T ~ 30K
  • 11. Estimate of Evaporation Time At 30 K, background photons: nγ ∼ 106cm-3, λ= 10-2cm. ΔE= pγ2 2m=(h/λ)22m ΔE ~ 10-34ergs/collision Given a cross-section, σ = 10−2 σ, for the interaction of silica with these photons, the rate of increase of the kinetic energy of a trapped particle is: dEdt=ΔEnγσc dE/dt ~ 10-26ergs/sec Integrating and evaluating for a 1 micron-sized particle, we get: τevap=4παmλ2h2nγσc2Iτevap≈1.5×108Isec where Iis expressed in Watts/m2. A respectable number: about 5 yearsfor I = 1 Watt/m2and ~ months for currently available laser intensities. with radius ~a: Particle size is critical. 100 nm-sized particles --τevap~ hours, will need damping.
  • 12. Consider all fields: Incident and scattered, Near and farPair of oscillators: Driven by fields andradiating like dipolesSolve for self-consistencyOptical Binding Force
  • 13. Optical Binding Potential Induced dipole moments in adjacent spheres will give rise to electromagnetic forces between the spheres. Burns, et al. give an approximation for this interaction energy: long-range interaction which oscillates in sign at λand falls off as 1/r. Calculations of this two-particle binding potential look encouraging. However, results are based on approximations not necessarily valid in theregime where particle radius ~ λ. Need to explore this effect with no approximations, i.e., in theMiescattering regime.
  • 15. One-and Two-Dimensional Traps20 20 μμmm20 20 μμmm 1500 traps2.8 2.8 μμmm2 2 μμmm 2 Beams 3 Beams
  • 16. Observation of optical binding and trapping in a Gaussian beam 1beam Auto-arrangement of 3 μm polystyrene beads at the waist of a Gaussian beam
  • 17. 2-Beam Interference Voltage supplyfiltersCCDpiezo- electric elementMOsample2 2 μμm beads in motorizedm motorizeddragged celldragged cellFringes translation withFringes withpiezopiezo--electric elementelectric element
  • 18. Optical Binding in 2-Beam Trap
  • 19. 3-Beam Interferencetemplategeneration intensity patternPiezoimagingsystemCCD
  • 20. Optical Binding in 3-Beam TrapJ.-M. Fournier, M.M. Burns, and J.A. Golovchenko, “Writing Diffractive Structures by Optical Trapping”, Proc. SPIE 2406 “Practical holography”,pp. 101-111, 1995. M.M. Burns, J.-M. Fournier, and J.A. Golovchenko, Optical Matter, US Patent # 5,245,466, 1993
  • 23. Force Calculation: Three Intersecting Plane Waves
  • 24. Project Goals Demonstrate and characterize a small, floating LTM in water. Develop and use computational algorithms to model an LTM which include all optical forces including optical binding effects. Combine lab measurements with particle design and the computational models to obtain estimates for the mirror stability and quality, and for the laser power requirements in a vacuum environment.
  • 25. Laser Trapped Mirrors in SpaceArtist’s view of Laser Trapped MirrorArtist’s Mirror(NASA study by Boeing(Boeing--SVS)