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NIAC 8th Annual Meeting: 2006 
Photon Tether Formation Flight (PTFF) Young K. Bae, Ph.D. Bae InstituteTustin, California, USAwww.baeinstitute.com
NIAC 8th Annual Meeting: 2006 
Participants 
zJoseph Carroll, Tether Applications Inc. 
--General Tether Aspects and Hardware 
zClaude Phipps, Ph.D., Photonics Associates 
--Nano-Newton Thruster Stand 
zEugene Levin, Ph.D., STARS, Inc. 
--Dynamics of Tethers and Formation Flying 
zBob Scaringe, AVG Communications 
--Business Development
NIAC 8th Annual Meeting: 2006 
Examples of Revolutionary/Disruptive Technologies 
Key Enabling Factor: 
Orders of Magnitude Enhancement in Critical Parameters 
zSubatomic Dimension --Particle Accelerators 
Critical Parameter: Particle Energy 
zAtomic Dimension –STM/AFM 
Critical Parameter: Scanning Ability/Noise Reduction 
zMolecular to Daily Life Dimension --Lasers 
Critical Parameter: Coherence of Photons 
zAstronomical Dimension –Precision Formation Flying (?) 
Critical Parameter: Control Accuracy (?)
NIAC 8th Annual Meeting: 2006 
Examples of Precision Formation Flying Concepts TPFSI MissionMAXIMLISASPECS
NIAC 8th Annual Meeting: 2006 
Selected Formation Flying Missions Control Accuracy Baseline Distance>1 km1 m1 mm1 mμ1 nm1 m10 m100 m1 km10 km100 km>1,000 kmGRACELISAPTFFSNAP 1TsinghuaESA Proba-3XEUSDARWINGEMINIMAXIMTechSat 21FTXRSPECSControl Limitation with Conventional Thrusters?
NIAC 8th Annual Meeting: 2006 
Nano-Meter Precision Spacecraft Formation Flying: --is able to cover most of critical missions planned--enables many other new missions•Thus, it is Potentially a Revolutionary/Disruptive Technology of the 21stCentury in Astronomical Dimension. •So far, its Enabling Technology has been illusive. •We believe that PTFF could be the Enabling Technology, if successfully demonstrated. •The Primary Goal of this NIAC Phase II is to demonstratea sub-scale prototype PTFF engine.
NIAC 8th Annual Meeting: 2006 
Photon Tether Formation Flight (PTFF) 
zForce Structure: Counter Balance of Two Forces: 
Contracting Force: Tether Tension 
Extending Force: Photon Thrust 
-Intracavity Arrangement 
-Thrust Multiplied by Tens of Thousand Times by Bouncing Photons between Spacecraft 
zGeometrical Structure: Crystalline Structure 
zInterspacecraftDistance Accuracy: better than nm 
zMaximum Operation Range: Tens of kms(Limited by Laser Mirror Size) 
zCan be Used for both Static and Dynamic Applications
NIAC 8th Annual Meeting: 2006 
Major Advantages of PTFF 
zUltra-High Baseline and Pointing Accuracy 
--Baseline Accuracy: better than 1 Nano-Meter 
--Pointing Accuracy: better than 0.1 micro-arcsecfor 1 km baseline system 
–Enabling Wide Ranges of Imaging Missions 
zPropellantless 
--System Mass Savings, Contamination Free, Long Mission Lifetime 
zLow Power Consumption 
zLow Construction Cost 
zDual Usage of Photon Thruster Laser for Interferometric Ranging System 
--Simplified System Architecture and Control, Low System Weight 
zReadily Downscalableto Nano-and Pico-Satellites Usage 
--Ideal for Sophisticated Fractionated Spacecraft or Space Structures
NIAC 8th Annual Meeting: 2006 
PTFF System ArchitectureSatellite ISatellite IIPrecision Laser Power MeterHR MirrorHR MirrorLaser Gain MediaUltrahigh Precision CW Photon ThrustTetherTensionPiezo-TranslatorStepper MotorIntracavity Laser BeamTetherReelClampLensDiodePumpLaserPumpLaser BeamHR MirrorHR MirrorPartal MirroriPhotodetectorPartal MirroriPartal MirroriTether SystemPhoton ThrusterSystemInterferometricRanging SystemNano-Precision Formation Flying System Architecture
NIAC 8th Annual Meeting: 2006 
Photon Thruster System: TRL 3Satellite ISatellite IIPrecision Laser Power MeterHR MirrorHR MirrorLaser Gain MediaUltrahigh Precision CW Photon ThrustIntracavity Laser BeamLensDiodePumpLaserPumpLaser Beam 
zLaser System 
--Diode Pumped Intracavity Laser 
--Lifetime of Diodes 
1 Year for Continuous Operation 
zPump Diode Carousel Design –Tens of Years
NIAC 8th Annual Meeting: 2006 
101001000100001000000.111010010001000010 W System Intracavity Photon Thrust as a Function of the Mirror Reflectance (R) Photon Thrust (μN) 11 - ROff-the-ShelfSuper MirrorPredicted Capability of the Proposed System
NIAC 8th Annual Meeting: 2006 
Specific thrusts as functions of Ispof various conventional and photon thrusters. Isp (sec) 102103104105106107108 Specific Thrust (mN/W) 10-710-610-510-410-310-210-1100X 1,000X 10,000X 100X 20,000Electric ThrustersPhoton ThrustersIntracavity Multiplication Factors
NIAC 8th Annual Meeting: 2006 
Intersatellite Distance (km) 0.010.1110100 Mirror Diamter (cm) 110Photon Thruster System: Mirror Diameter vs. Operation Distance
NIAC 8th Annual Meeting: 2006 
Interferometric Ranging System: TRL 5Satellite ISatellite IIPrecision Laser Power MeterHR MirrorHR MirrorLaser Gain MediaUltrahigh Precision CW Photon ThrustIntracavity Laser BeamLensDiodePumpLaserPumpLaser BeamHR MirrorHR MirrorPartal MirroriPhotodetectorPartal MirroriPartal Mirrori 
zDual Usage of Photon Thruster Laser for Interferometric Ranging System Source Laser 
--System Architecture Simplification 
--System Mass Reduction
NIAC 8th Annual Meeting: 2006 
Heterodyne Interferometric Ranging System Integrated with PhotonThruster SystemSatellite ISatellite IIPrecision Laser Power MeterHR MirrorHR MirrorLaser Gain MediaUltrahigh Precision CW Photon ThrustIntracavity Laser BeamLensDiodePumpLaserPumpLaser BeamPartal MirroriBeam SplitterMeasurementDetectorReferenceDetectorAOMAOMRetroreflectorMirrorODL
NIAC 8th Annual Meeting: 2006 
Tether System: TRL 5Satellite ISatellite IITetherClampTetherReelInchwormPiezo-TranslatorElectromechnical Damper 
zCoarse Control: Reel System--mm Accuracy 
zFine Control: Inchworm or Stepper Motor--μm Accuracy 
zUltrafineControl: Piezo-Translator (off-the-shelf) --0.1 nm Accuracy
NIAC 8th Annual Meeting: 2006 
Method of Tether Vibration Suppression•Major Tether Vibrations will Result from Reorientation of the Whole Formation Structure, and other Sudden Environmental Perturbations, such as Meteoroid Impacts. •Longitudinal Tether Wave DampingTether Material Friction/ Modulation of Photon Thruster Power•Transverse Tether Wave DampingElectromechanical Damper with Impedance MatchingDamping Applied 
Electromechanical Damping 
Simulation by Lorenziniet al. 
For 1 km Baseline System
NIAC 8th Annual Meeting: 2006 
Example I: 10 km 1-D PTFF at L2
NIAC 8th Annual Meeting: 2006 
Example II: 1 km PTFF Telescope at L2
NIAC 8th Annual Meeting: 2006 
1 km PTFF Telescope: Enables New World Imager Freeway MissionBy Prof. W. Cash –2005 NIAC Fellow Meeting--Searching for Advanced Civilization in Exo-Planets•300 m resolution at 10 parsecs = 0.02 nano-arcseconds•500,000 km based line distance between Collectors•Huge collecting area –one square kilometer
NIAC 8th Annual Meeting: 2006 
More Advanced PTFF TelescopeJames WebbSpace TelescopeStretched Membrane Mirror (NIAC)Image Processing With Real-TimeHolographic AberrationCorrection (NIAC)
NIAC 8th Annual Meeting: 2006 
Technology Readiness Assessment Summary 
zPhoton Thrusters: TRL 3 
zInterferometric Ranging System: TRL 5 
zTether System: TRL 5 
zSystem Integration and Control: TRL 2 
zR&D3:II -III (moderate -high) (Degree of Difficulty) 
--Requires to optimize photon thrust design based on the current laboratory system and system integration, and to develop control system.
NIAC 8th Annual Meeting: 2006 
Phase II Work Started Since Sept. 1st2006 
zProof-of-Concept Demonstration of Photon Thruster 
zConstruction of a Thrust Stand with nNAccuracy 
zOverall System Stability and Control 
zTether Vibration Dynamics 
zEnvironment Perturbation 
z3-D Simulation 
zDesign of Prototype Interferometric Ranging System 
zDesign of Prototype Tether System 
zDetailed Study of Specific Applications 
zIn-Depth Revisits of Existing Concepts --SPECS and MAXIM 
zUltralargeMembrane Space Telescopes 
zUltralargeSparse Aperture Space Telescopes 
zOthers
NIAC 8th Annual Meeting: 2006 
Prototype Sub-scale PTFF Engine Demonstration Laser Power MeterConcave HR MirrorHR MirrorLaser MediaTorsionFiberCounterWeightVacuum ChamberInterference PatternLow Power LaserCorner CubeWindowsOptical FiberPhoto Detectorfor Fringe MonitoringPump Laser DiodePiezo-TranslatorTetherIntracavity Laser BeamComputerFeedbackElectronics
NIAC 8th Annual Meeting: 2006 
Conclusions I 
zIf successful, PTFF technology will be revolutionary/disruptive technology of 21stCentury in Astronomical Dimension. 
zIf successful, PTFF technology will open new innovative (revolutionary) ways to implementing new and existing mission concepts at very affordable costs. --Many applications can be implemented at fractional costs of HST. 
zPreliminary Studies concluded that PTFF system can be implemented with off-the-shelf technologies –This will be tried to be proved during this study.
NIAC 8th Annual Meeting: 2006 
Conclusions II 
•Mission Specific Applications•PTFF Simplifies the Architecture and Reduces the Weight inSpace InterferometeryMissions --TPF, DARWIN, MAXIM, SPECS, FTXR etc. •Ultra-large PTFF Space Telescopes --For New World Imager (300 m Resolution –Freeway Mission with km Mirror) --Earth imaging/Monitoring/Surveillance (10 cm ResolutionMonitoring at GEO with 200 m Mirror)
NIAC 8th Annual Meeting: 2006 
“I believe in intuitions and inspirations. I sometimes feel that I am right. I do not know that I am.” by Albert EinsteinThe Support by NIACand NASAfor this project is greatly appreciated.

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1374 bae[1]

  • 1. NIAC 8th Annual Meeting: 2006 Photon Tether Formation Flight (PTFF) Young K. Bae, Ph.D. Bae InstituteTustin, California, USAwww.baeinstitute.com
  • 2. NIAC 8th Annual Meeting: 2006 Participants zJoseph Carroll, Tether Applications Inc. --General Tether Aspects and Hardware zClaude Phipps, Ph.D., Photonics Associates --Nano-Newton Thruster Stand zEugene Levin, Ph.D., STARS, Inc. --Dynamics of Tethers and Formation Flying zBob Scaringe, AVG Communications --Business Development
  • 3. NIAC 8th Annual Meeting: 2006 Examples of Revolutionary/Disruptive Technologies Key Enabling Factor: Orders of Magnitude Enhancement in Critical Parameters zSubatomic Dimension --Particle Accelerators Critical Parameter: Particle Energy zAtomic Dimension –STM/AFM Critical Parameter: Scanning Ability/Noise Reduction zMolecular to Daily Life Dimension --Lasers Critical Parameter: Coherence of Photons zAstronomical Dimension –Precision Formation Flying (?) Critical Parameter: Control Accuracy (?)
  • 4. NIAC 8th Annual Meeting: 2006 Examples of Precision Formation Flying Concepts TPFSI MissionMAXIMLISASPECS
  • 5. NIAC 8th Annual Meeting: 2006 Selected Formation Flying Missions Control Accuracy Baseline Distance>1 km1 m1 mm1 mμ1 nm1 m10 m100 m1 km10 km100 km>1,000 kmGRACELISAPTFFSNAP 1TsinghuaESA Proba-3XEUSDARWINGEMINIMAXIMTechSat 21FTXRSPECSControl Limitation with Conventional Thrusters?
  • 6. NIAC 8th Annual Meeting: 2006 Nano-Meter Precision Spacecraft Formation Flying: --is able to cover most of critical missions planned--enables many other new missions•Thus, it is Potentially a Revolutionary/Disruptive Technology of the 21stCentury in Astronomical Dimension. •So far, its Enabling Technology has been illusive. •We believe that PTFF could be the Enabling Technology, if successfully demonstrated. •The Primary Goal of this NIAC Phase II is to demonstratea sub-scale prototype PTFF engine.
  • 7. NIAC 8th Annual Meeting: 2006 Photon Tether Formation Flight (PTFF) zForce Structure: Counter Balance of Two Forces: Contracting Force: Tether Tension Extending Force: Photon Thrust -Intracavity Arrangement -Thrust Multiplied by Tens of Thousand Times by Bouncing Photons between Spacecraft zGeometrical Structure: Crystalline Structure zInterspacecraftDistance Accuracy: better than nm zMaximum Operation Range: Tens of kms(Limited by Laser Mirror Size) zCan be Used for both Static and Dynamic Applications
  • 8. NIAC 8th Annual Meeting: 2006 Major Advantages of PTFF zUltra-High Baseline and Pointing Accuracy --Baseline Accuracy: better than 1 Nano-Meter --Pointing Accuracy: better than 0.1 micro-arcsecfor 1 km baseline system –Enabling Wide Ranges of Imaging Missions zPropellantless --System Mass Savings, Contamination Free, Long Mission Lifetime zLow Power Consumption zLow Construction Cost zDual Usage of Photon Thruster Laser for Interferometric Ranging System --Simplified System Architecture and Control, Low System Weight zReadily Downscalableto Nano-and Pico-Satellites Usage --Ideal for Sophisticated Fractionated Spacecraft or Space Structures
  • 9. NIAC 8th Annual Meeting: 2006 PTFF System ArchitectureSatellite ISatellite IIPrecision Laser Power MeterHR MirrorHR MirrorLaser Gain MediaUltrahigh Precision CW Photon ThrustTetherTensionPiezo-TranslatorStepper MotorIntracavity Laser BeamTetherReelClampLensDiodePumpLaserPumpLaser BeamHR MirrorHR MirrorPartal MirroriPhotodetectorPartal MirroriPartal MirroriTether SystemPhoton ThrusterSystemInterferometricRanging SystemNano-Precision Formation Flying System Architecture
  • 10. NIAC 8th Annual Meeting: 2006 Photon Thruster System: TRL 3Satellite ISatellite IIPrecision Laser Power MeterHR MirrorHR MirrorLaser Gain MediaUltrahigh Precision CW Photon ThrustIntracavity Laser BeamLensDiodePumpLaserPumpLaser Beam zLaser System --Diode Pumped Intracavity Laser --Lifetime of Diodes 1 Year for Continuous Operation zPump Diode Carousel Design –Tens of Years
  • 11. NIAC 8th Annual Meeting: 2006 101001000100001000000.111010010001000010 W System Intracavity Photon Thrust as a Function of the Mirror Reflectance (R) Photon Thrust (μN) 11 - ROff-the-ShelfSuper MirrorPredicted Capability of the Proposed System
  • 12. NIAC 8th Annual Meeting: 2006 Specific thrusts as functions of Ispof various conventional and photon thrusters. Isp (sec) 102103104105106107108 Specific Thrust (mN/W) 10-710-610-510-410-310-210-1100X 1,000X 10,000X 100X 20,000Electric ThrustersPhoton ThrustersIntracavity Multiplication Factors
  • 13. NIAC 8th Annual Meeting: 2006 Intersatellite Distance (km) 0.010.1110100 Mirror Diamter (cm) 110Photon Thruster System: Mirror Diameter vs. Operation Distance
  • 14. NIAC 8th Annual Meeting: 2006 Interferometric Ranging System: TRL 5Satellite ISatellite IIPrecision Laser Power MeterHR MirrorHR MirrorLaser Gain MediaUltrahigh Precision CW Photon ThrustIntracavity Laser BeamLensDiodePumpLaserPumpLaser BeamHR MirrorHR MirrorPartal MirroriPhotodetectorPartal MirroriPartal Mirrori zDual Usage of Photon Thruster Laser for Interferometric Ranging System Source Laser --System Architecture Simplification --System Mass Reduction
  • 15. NIAC 8th Annual Meeting: 2006 Heterodyne Interferometric Ranging System Integrated with PhotonThruster SystemSatellite ISatellite IIPrecision Laser Power MeterHR MirrorHR MirrorLaser Gain MediaUltrahigh Precision CW Photon ThrustIntracavity Laser BeamLensDiodePumpLaserPumpLaser BeamPartal MirroriBeam SplitterMeasurementDetectorReferenceDetectorAOMAOMRetroreflectorMirrorODL
  • 16. NIAC 8th Annual Meeting: 2006 Tether System: TRL 5Satellite ISatellite IITetherClampTetherReelInchwormPiezo-TranslatorElectromechnical Damper zCoarse Control: Reel System--mm Accuracy zFine Control: Inchworm or Stepper Motor--μm Accuracy zUltrafineControl: Piezo-Translator (off-the-shelf) --0.1 nm Accuracy
  • 17. NIAC 8th Annual Meeting: 2006 Method of Tether Vibration Suppression•Major Tether Vibrations will Result from Reorientation of the Whole Formation Structure, and other Sudden Environmental Perturbations, such as Meteoroid Impacts. •Longitudinal Tether Wave DampingTether Material Friction/ Modulation of Photon Thruster Power•Transverse Tether Wave DampingElectromechanical Damper with Impedance MatchingDamping Applied Electromechanical Damping Simulation by Lorenziniet al. For 1 km Baseline System
  • 18. NIAC 8th Annual Meeting: 2006 Example I: 10 km 1-D PTFF at L2
  • 19. NIAC 8th Annual Meeting: 2006 Example II: 1 km PTFF Telescope at L2
  • 20. NIAC 8th Annual Meeting: 2006 1 km PTFF Telescope: Enables New World Imager Freeway MissionBy Prof. W. Cash –2005 NIAC Fellow Meeting--Searching for Advanced Civilization in Exo-Planets•300 m resolution at 10 parsecs = 0.02 nano-arcseconds•500,000 km based line distance between Collectors•Huge collecting area –one square kilometer
  • 21. NIAC 8th Annual Meeting: 2006 More Advanced PTFF TelescopeJames WebbSpace TelescopeStretched Membrane Mirror (NIAC)Image Processing With Real-TimeHolographic AberrationCorrection (NIAC)
  • 22. NIAC 8th Annual Meeting: 2006 Technology Readiness Assessment Summary zPhoton Thrusters: TRL 3 zInterferometric Ranging System: TRL 5 zTether System: TRL 5 zSystem Integration and Control: TRL 2 zR&D3:II -III (moderate -high) (Degree of Difficulty) --Requires to optimize photon thrust design based on the current laboratory system and system integration, and to develop control system.
  • 23. NIAC 8th Annual Meeting: 2006 Phase II Work Started Since Sept. 1st2006 zProof-of-Concept Demonstration of Photon Thruster zConstruction of a Thrust Stand with nNAccuracy zOverall System Stability and Control zTether Vibration Dynamics zEnvironment Perturbation z3-D Simulation zDesign of Prototype Interferometric Ranging System zDesign of Prototype Tether System zDetailed Study of Specific Applications zIn-Depth Revisits of Existing Concepts --SPECS and MAXIM zUltralargeMembrane Space Telescopes zUltralargeSparse Aperture Space Telescopes zOthers
  • 24. NIAC 8th Annual Meeting: 2006 Prototype Sub-scale PTFF Engine Demonstration Laser Power MeterConcave HR MirrorHR MirrorLaser MediaTorsionFiberCounterWeightVacuum ChamberInterference PatternLow Power LaserCorner CubeWindowsOptical FiberPhoto Detectorfor Fringe MonitoringPump Laser DiodePiezo-TranslatorTetherIntracavity Laser BeamComputerFeedbackElectronics
  • 25. NIAC 8th Annual Meeting: 2006 Conclusions I zIf successful, PTFF technology will be revolutionary/disruptive technology of 21stCentury in Astronomical Dimension. zIf successful, PTFF technology will open new innovative (revolutionary) ways to implementing new and existing mission concepts at very affordable costs. --Many applications can be implemented at fractional costs of HST. zPreliminary Studies concluded that PTFF system can be implemented with off-the-shelf technologies –This will be tried to be proved during this study.
  • 26. NIAC 8th Annual Meeting: 2006 Conclusions II •Mission Specific Applications•PTFF Simplifies the Architecture and Reduces the Weight inSpace InterferometeryMissions --TPF, DARWIN, MAXIM, SPECS, FTXR etc. •Ultra-large PTFF Space Telescopes --For New World Imager (300 m Resolution –Freeway Mission with km Mirror) --Earth imaging/Monitoring/Surveillance (10 cm ResolutionMonitoring at GEO with 200 m Mirror)
  • 27. NIAC 8th Annual Meeting: 2006 “I believe in intuitions and inspirations. I sometimes feel that I am right. I do not know that I am.” by Albert EinsteinThe Support by NIACand NASAfor this project is greatly appreciated.