TPF-I SWG Report - Exoplanet Exploration Program - NASA

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A PPENDIX D NaCl NAR NASA NASTRAN Ne NGST NICMOS nm N 2 O NRA NRL NTP sodium chloride Non-Advocate Review National Aeronautics and Space Administration NASA Structural Analysis Program neon Northrop Grumman Space Technology Near Infrared Camera and Multi-Object Spectrometer nanometer (10 -9 meters) nitrous oxide NASA Research Announcement Naval Research Laboratory Network Time Protocol O 2 O 3 oxygen ozone OB association association of spectral class O and B stars ObSim Observatory Simulation model OPD optical path difference OASES Outpost for the Analysis and Spectroscopy of Exoplanetary Systems OPD optical path difference OWA outer working angle PAH PAL pc PCI PDR PDT PI PMSR POP ppb PPS PRIMA PSD PSE PSF PSR P-V QE R&A RCS RF RFI RFP RMS, rms R/T RTC 192 polycyclic aromatic hydrocarbons present atmospheric level parsec (3.259 light-years, or 30.83 × 10 12 km) peripheral communications interconnect local bus Preliminary Design Review Planet Detection Testbed principal investigator Preliminary Mission Systems Review Program Operating Plan parts per billion pulse per second Phase-Referenced Imaging and Micro-arcsecond Astrometry power spectral density planetary signal extraction point spread function Pre-Ship Review peak to valley quantum efficiency research and analysis Reaction Control System radio frequency Request For Information Request for Proposal root mean-square near reflection/transmission (ratio) relative thermal constraint
A C R O N Y M S RWA S SAC SBIR SCI SCI SCLKs SCUBA SE Si:As SiC SIRTF SIM S/N SNR SPIE SWG TAU TCL TCP/IP TDMA TMA TOM TOO TPF TPF-C TPF-I TRL TRP TSC UA UDP u-v VLA VLT V&V WFE WFS WFS&C WIIT YSO reaction wheel assembly sulfur Sun-avoidance constraint Small Business Innovative Research structurally connected interferometer Scalable Coherent Interface (protocol) simulation of local spacecraft clocks Submillimetre Common-User Bolometer Array (on the JCMT in Hawaii) Software Executive silicon:arsenic silicon carbide Space Infrared Telescope Facility (now Spitzer Space Telescope) Space Interferometry Mission signal-to-noise ratio signal-to-noise ratio International Society for Optical Engineering Science Working Group Tel Aviv University Tool Command Language transmission control protocol/internet protocol time division multiple access tertiary mirror assembly thermo-optical mechanical target of opportunity Terrestrial Planet Finder Terrestrial Planet Finder Coronagraph Terrestrial Planet Finder Interferometer technology readiness level Technology Review Panel thruster synchronization constraint University of Arizona user datagram protocol spatial frequency coordinates, in wavelengths Very Large Array, National Radio Astronomy Observatory Very Large Telescope, European Southern Observatory verification and validation wavefront error wavefront sensor wavefront sensing and control Wide-field Imaging Interferometry Testbed young stellar objects 193
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JPL Publication 07-1 Terrestrial Pl
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Abstract Over the past two years, t
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Acknowledgements Twenty-two represe
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Table of Contents 1 Introduction...
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4.8.3 Post-Nulling Calibration.....
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6.4.5 Double Fourier Interferometry
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I NTRODUCTION 1 Introduction Over 2
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I NTRODUCTION et al. 2004), and res
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I NTRODUCTION Standard Interferomet
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I NTRODUCTION 1.4 References Angel,
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C HAPTER 2 0.7 to 1.5 AU scaled by
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C HAPTER 2 Table 2-2. Illustrative
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C HAPTER 2 Classical interferometry
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C HAPTER 2 trivial in the absence o
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C HAPTER 2 Figure 2-3. Simulated mi
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C HAPTER 2 would be in atmospheres
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C HAPTER 2 Figure 2-6. The mid-infr
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C HAPTER 2 Lines of constant stella
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C HAPTER 2 presence of zodiacal clo
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C HAPTER 2 S EZ 2π ∫ θ max ∫
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C HAPTER 2 Figure 2-11. Observation
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C HAPTER 2 Figure 2-12. Models of t
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C HAPTER 2 Beichman, C. A., Fridlun
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C HAPTER 2 2.7.4 Suitable Targets E
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C HAPTER 2 Reach, W. T., Franz, B.
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C HAPTER 3 3.1.1 Darwin/TPF-I Prope
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C HAPTER 3 clouds or an OB associat
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C HAPTER 3 Figure 3-3. Three possib
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C HAPTER 3 the circumstellar disk,
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C HAPTER 3 Figure 3-6. (Left panel)
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C HAPTER 3 Continuum interferometry
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C HAPTER 3 Figure 3-9: Simulated im
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C HAPTER 3 3.3 Conclusions Darwin/T
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C HAPTER 3 Nguyen, H. T., Kallivaya
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D ESIGN AND A R C H I T E C T U R E
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C HAPTER 5 Heavy launch vehicle. Th
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C HAPTER 5 5.3.2 Combiner Spacecraf
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C HAPTER 5 5.3.5 Beam Transfer betw
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C HAPTER 5 Figure 5-8. Control sche
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C HAPTER 5 Figure 5-9. First sectio
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C HAPTER 5 Figure 5-9 shows the fir
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C HAPTER 5 5.4.4 Shear Metrology Sh
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C HAPTER 5 Figure 5-15. TPF-I Fligh
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C HAPTER 5 secondary mirror along t
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C HAPTER 5 a) c) b) d) IWA = 43 mas
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C HAPTER 5 planets found. Figure 5-
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C HAPTER 5 30 25 5 M earth 3 M eart
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C HAPTER 5 5.8.4 Angular Resolution
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C HAPTER 5 Table 5-3. Angular Resol
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C HAPTER 5 The optimization works b
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T E C H N O L O G Y R OADMAP FOR TP
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Page 155 and 156: T E C H N O L O G Y R OADMAP FOR TP
Page 173 and 174: F UTURE D EVELOPMENTS 7 Preparatory
Page 175 and 176: F UTURE D EVELOPMENTS • To comple
Page 177 and 178: F UTURE D EVELOPMENTS Table 7-1. Pr
Page 179 and 180: D ISCUSSION AND C ONCLUSION 8 Discu
Page 181 and 182: Appendices 167
Page 183 and 184: T E C H N O L O G Y A DVISORY C O M
Page 185 and 186: F L I G H T S YSTEM C ONFIGURATION
Page 187: F L I G H T S YSTEM C ONFIGURATION
Page 190 and 191: A PPENDIX C 2. Identical FACS fligh
Page 192 and 193: A PPENDIX C 2. Recall that the coef
Page 194 and 195: A PPENDIX C Once the formation has
Page 196 and 197: A PPENDIX C Figure C-3. Example of
Page 198 and 199: A PPENDIX C Figure C-4. FAST Flight
Page 200 and 201: A PPENDIX C The “true” time of
Page 202 and 203: A PPENDIX C References Cohen, S., a
Page 204 and 205: A PPENDIX D DC DCB DM DM DOCS DOD D
Page 208 and 209: A PPENDIX E Appendix E TPF-I Review
Page 210 and 211: A PPENDIX F Alice Quillen, Universi
Page 212: A PPENDIX F Figure 3-1 - Original f
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