Starshade is one of the technologies that will enable the observation and characterization of small planets around nearby stars through direct imaging. Extensive models have been developed to describe a starshade’s optical performance and noise budget in exoplanet imaging. The Starshade Exoplanet Data Challenge was designed to validate this noise budget and evaluate the capabilities of image-processing techniques by inviting community participating teams to analyze >1000 simulated images of hypothetical exoplanetary systems observed through a starshade. Because the starshade would suppress the starlight so well, the dominant noise source remaining in the images becomes the exozodiacal disks and their structures. We summarize the techniques used by the participating teams and compare their findings with the truth. With an independent component analysis to remove the background, ∼70% of the inner planets (close to the inner working angle) have been detected along with ∼30% of the outer planets. Planet detection becomes more difficult in the cases of higher disk inclination as the false negative and false positive counts increase. Interestingly, we found little difference in the planet detection rate between 10−10 and 10−9 instrument contrast, confirming that the dominant limitations are from the astrophysical background and not the performance of the starshade. A non-parametric background calibration scheme, such as the independent component analysis reported here, results in a mean residual of 10% the background brightness. This background estimation error leads to substantial false positives and negatives and systematic bias in the planet flux estimation and should be included in the estimation of the planet detection signal-to-noise ratio for imaging using a starshade and also a coronagraph that delivers exozodi-limited imaging. These results corroborate the starshade noise budget and provide new insight into background calibration that will be useful for anticipating the science capabilities of future high-contrast imaging space missions.
Starshade is one of the technologies that will enable the observation and characterization of small planets around solar-like stars through direct imaging. Extensive models have been developed to describe a starshade's optical performance and the resulting noise budget in exoplanet imaging. The Starshade Exoplanetary Data Challenge (SEDC) was designed to validate this noise budget and evaluate the capabilities of image-processing techniques, by inviting community participating teams to analyze >1000 simulated images of hypothetical exoplanetary systems observed through a starshade. One of the biggest challenges of the planetary discovery through the direct image technique is the distinction between true planets and structures in exozodiacal disks. Here we summarize the techniques used by the participating teams and compare their findings with the truth. With an independent component analysis to remove the background, about 70% of the inner planets (close to the inner working angle) have been detected and ~40 of the outer planet (fainter than the inner counterparts) have been identified. Also, the inclination of the exozodiacal disk can be inferred from individual images. Planet detection becomes more difficult in the cases of higher disk inclination, as the false negative and false positive numbers increase. Finally, we find that a non-parametric background calibration scheme, such as the independent component analysis reported here, can perform background subtraction close to the photon-noise limit, with a median residual of ~5% the background brightness, for exozodiacal density level ranging between 1 and 30 zodis. The results of the SEDC strongly corroborate the starshade noise budget with realistic images, and provide new insight into background calibration that will be useful for anticipating the science capabilities of future missions that use a starshade.
The CANDLE Engineering Demonstration Unit (EDU) was selected by the 2022 APRA program to develop and demonstrate the ability to reach the flux accuracy and range required for an artificial flux calibration star. A critical issue in producing accurate and reliable flux calibration is systematic effects; this EDU is providing a path to deploying an artificial star calibration payload outside Earth’s atmosphere with SI-traceable calibration that enables accurate throughput characterization of astronomical and earth science observatories in space and on the ground. Such a payload could be carried independently on a dedicated platform such as an orbiting satellite, e.g. the Orbiting Configurable Artificial Star (ORCAS), by a star shade at L2, or some other independent platform to enable accurate end-to-end throughput vs. wavelength calibration that can be measured repeatedly throughout the operational lifetime of an observatory. Once calibrated, the observatory is enabled to carry out astrophysical programs whose science objectives demand high accuracy and/or high precision observations. One specific and immediate application is establishing SI-traceable standard stars beyond the current limited set. We show in this paper the progress made in developing this EDU.
We have built and commissioned a prototype agitated non-circular core ber scrambler for precision spectroscopic radial velocity measurements in the near-infrared H band. We have collected the rst on-sky performance and modal noise tests of these novel bers in the near-infrared at H and K bands using the CSHELL spectrograph at the NASA InfraRed Telescope Facility (IRTF). We discuss the design behind our novel reverse injection of a red laser for co-alignment of star-light with the ber tip via a corneWe have built and commissioned a prototype agitated non-circular core fiber scrambler for precision spectroscopic radial velocity measurements in the near-infrared H band. We have collected the first on-sky performance and modal noise tests of these novel fibers in the near-infrared at H and K bands using the CSHELL spectrograph at the NASA InfraRed Telescope Facility (IRTF). We discuss the design behind our novel reverse injection of a red laser for co-alignment of star-light with the fiber tip via a corner cube and visible camera. We summarize the practical details involved in the construction of the fiber scrambler, and the mechanical agitation of the fiber at the telescope. We present radial velocity measurements of a bright standard star taken with and without the fiber scrambler to quantify the relative improvement in the obtainable blaze function stability, the line spread function stability, and the resulting radial velocity precision. We assess the feasibility of applying this illumination stabilization technique to the next generation of near-infrared spectrographs such as iSHELL on IRTF and an upgraded NIRSPEC at Keck. Our results may also be applied in the visible for smaller core diameter fibers where Fiber modal noise is a significant factor, such as behind an adaptive optics system or on a small < 1 meter class telescope such as is being pursued by the MINERVA and LCOGT collaborations.r cube and visible camera. We summarize the practical details involved in the construction of the ber scrambler, and the mechanical agitation of the ber at the telescope. We present radial velocity measurements of a bright standard star taken with and without the ber scrambler to quantify the relative improvement in the obtainable blaze function stability, the line spread function stability, and the resulting radial velocity precision. We assess the feasibility of applying this illumination stabilization technique to the next generation of near-infrared spectrographs such as iSHELL on IRTF and an upgraded NIRSPEC at Keck. Our results may also be applied in the visible for smaller core diameter bers where ber modal noise is a signi cant factor, such as behind an adaptive optics system or on a small < 1 meter class telescope such as is being pursued by the MINERVA and LCOGT collaborations.
We have built and commissioned gas absorption cells for precision spectroscopic radial velocity measurements in the near-infrared in the H and K bands. We describe the construction and installation of three such cells filled with 13CH4, 12CH3D, and 14NH3 for the CSHELL spectrograph at the NASA Infrared Telescope Facility (IRTF). We have obtained their high-resolution laboratory Fourier Transform spectra, which can have other practical uses. We summarize the practical details involved in the construction of the three cells, and the thermal and mechanical control. In all cases, the construction of the cells is very affordable. We are carrying out a pilot survey with the 13CH4 methane gas cell on the CSHELL spectrograph at the IRTF to detect exoplanets around low mass and young stars. We discuss the current status of our survey, with the aim of photon-noise limited radial velocity precision. For adequately bright targets, we are able to probe a noise floor of 7 m/s with the gas cell with CSHELL at cassegrain focus. Our results demonstrate the feasibility of using a gas cell on the next generation of near-infrared spectrographs such as iSHELL on IRTF, iGRINS, and an upgraded NIRSPEC at Keck.
The New Worlds, New Horizons report released by the Astronomy and Astrophysics Decadal Survey Board in 2010
listed the Wide Field Infrared Survey Telescope (WFIRST) as the highest-priority large space mission for the coming
decade. This observatory will provide wide-field imaging and slitless spectroscopy at near infrared wavelengths. The
scientific goals are to obtain a statistical census of exoplanets using gravitational microlensing, measure the expansion
history of and the growth of structure in the Universe by multiple methods, and perform other astronomical surveys to be
selected through a guest observer program. A Science Definition Team has been established to assist NASA in the
development of a Design Reference Mission that accomplishes this diverse array of science programs with a single
observatory. In this paper we present the current WFIRST payload concept and the expected capabilities for planet
detection. The observatory, with science goals that are complimentary to the Kepler exoplanet transit mission, is
designed to complete the statistical census of planetary systems in the Galaxy, from habitable Earth-mass planets to free
floating planets, including analogs to all of the planets in our Solar System except Mercury. The exoplanet microlensing
survey will observe for 500 days spanning 5 years. This long temporal baseline will enable the determination of the
masses for most detected exoplanets down to 0.1 Earth masses.
SIM PlanetQuest is a space-borne Michelson interferometer with a nine meter baseline that will survey ~200 stars
within 30 parsecs for terrestrial mass planets. Ultra-precise astrometric observations will reveal the gravitational wobble
of the target star (due to a planetary companion) against an inertial frame of reference stars located within a 1.5 degree
radius. Here, we report the results of multiple Monte Carlo simulations which have modeled SIM's ability to detect and
determine the orbital parameters and masses of the terrestrial mass planets around its potential sample of target stars.
We find that SIM will detect 80% of the planets in the 60 star sample. Out of those planets SIM detects, we will be able
to estimate the masses of at least 50% of the planets to 30%. Whether SIM should observer 60 or 240 stars, will be
aided by the results of the Kepler mission which will provide statistics on the frequency of terrestrial-mass planets
around solar type stars. By determining the orbital phase of the planet, SIM will be able to assist TPF-C by telling it
when to look to ensure that the planet will be outside the TPF-C 62 mas inner working angle. Furthermore, the masses
determined by SIM will not suffer from the msini ambiguity inherent in radial velocity surveys.
We present diffraction limited 2-25 micrometers images, obtained with the W.M. Keck 10-m telescopes that spatially resolve the cool Galactic Center source IRS 21, an enigmatic object that has alluded classification. Modeled as a Gaussian, the azimuthally averaged intensity profile of IRS 21, an enigmatic object that has alluded classification. Modeled asa a Gaussian, the azimuthally averaged intensity profile of IRS 21 has a HWHM radius of 740 +/- 30 AU at 2.2 micrometers and an average HWHM radius of 1540 +/- 90 AU at mid-IR wavelength. These sizes along with its color temperature favor the hypothesis that IRS 21 is self-luminous rather than an externally heated dust clump. Based on the size alone, the remaining possible dust geometries are (1) an intrinsic inflow or outflow or (2) an extrinsic dust distribution, in which case IRS 21 could be simply embedded in the Northern Arm. A simple SED model of the IR photometry from the literature and our mid-IR images reveal that the near-IR radiation is scattered light from an unknown embedded source while the mid-IR radiation is the remaining re-radiated light. The agreement between the 2.2 micrometers polarization angle for IRS 21 and the 12.5 micrometers polarization angle at the position of IRS 21, the symmetric shape of its intensity profiles, as well as the similarity of the observed properties of all the Northern Arm sources, lead us to conclude that the scattering dust around IRS 21 is extrinsic to the central source and is associated with the Northern Arm.
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