Proceedings of SPIE, the International Society for Optical Engineering/Proceedings of SPIE · 2012 · 24 citations · 20 references
Natural SciencesAerospace EngineeringPhysicsAstrodynamicsOpticsSpacecraft DesignAstrometric InstrumentationDetector TechnologyFlightInstrument Pointing StabilityMirror SystemsPayload RequirementsPointingPointing SystemsPrimary Mirror DesignSpacecraft Pointing Stability
The Planetary Imaging Concept Testbed Using a Rocket Experiment (PICTURE 36.225 UG) was designed to directly image the exozodiacal dust disk of ǫ Eridani (K2V, 3.22 pc) down to an inner radius of 1.5 AU. PICTURE carried four key enabling technologies on board a NASA sounding rocket at 4:25 MDT on October 8th, 2011: a 0.5 m light-weight primary mirror (4.5 kg), a visible nulling coronagraph (VNC) (600-750 nm), a 32x32 element MEMS deformable mirror and a milliarcsecond-class fine pointing system. Unfortunately, due to a telemetry failure, the PICTURE mission did not achieve scientific success. Nonetheless, this flight validated the flight-worthiness of the lightweight primary and the VNC. The fine pointing system, a key requirement for future planet-imaging missions, demonstrated 5.1 mas RMS in-flight pointing stability. We describe the experiment, its subsystems and flight results. We outline the challenges we faced in developing this complex payload and our technical approaches.
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A Dust Ring around ε Eridani: Analog to the Young Solar System
J. S. Greaves, W. S. Holland, G. H. Moriarty‐Schieven et al. · The Astrophysical Journal · 1998 · 333 citations · Full text
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The Palomar Testbed Interferometer
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A. P. Hatzes, William D. Cochran, B. McArthur et al. · The Astrophysical Journal · 2000 · 274 citations · Full text
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