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  • Astronomy
  • Electronics and Electrical Engineering
  • 2015-2019  (852)
  • 2005-2009  (1,845)
  • 1950-1954  (1)
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  • 1
    Publication Date: 2019-05-07
    Description: In order to tackle and solve the prediction problem of the lifetime of Li-ion batteries, it is essential to have awareness of the current state and health of the battery pack. To be able to accurately predict the future state of any system, one must possess knowledge of its current and future operations. Using derived models of the current and future system behavior, a model-based prognostics approach can be implemented as a solution to the prediction problem. As more and more autonomous electric vehicles progressively emerge in our daily life, a very critical challenge lies in accurate prediction of remaining useful life of the systems/subsystems. Batteries, power electronics conditioning systems, and motors are integrated to form the powertrain in electric vehicles; one of the most critical systems. In the case of electric aircrafts, computing remaining flying time is critical for safety, since an aircraft that runs out of power (battery charge) while in the air will eventually lose control leading to catastropheThis presentation covers a physics-based modeling approach implemented for case studies in capacitor and battery prognostics which are an integral part of an electrical powertrain system. The general approach of model-based prognostics will be examined as a potential solution for safety critical problems related to battery state of charge and state of health.
    Keywords: Electronics and Electrical Engineering
    Type: ARC-E-DAA-TN64822 , IEEE Power Electronics Society Lecture; Santa Clara, CA; United States
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  • 2
    Publication Date: 2019-06-06
    Description: Emerging power metal-oxide semiconductor field-effect transistor (MOSFETs) based on silicon carbide and gallium nitride technology are finding widespread use in many electronic applications such as motor control and DC/DC converters due to their higher voltage, higher temperature tolerance, and higher frequency switching capabilities. To utilize these power devices and to meet circuit/system compactness, modularity, and operational functionality, gate drivers that provide unique attributes, such as fast switching and high-current handling capability, are needed. In addition, power systems geared for use in space mission applications require on-board devices to withstand exposure to extreme temperatures and wide thermal swings. Very little data, however, exist on the performance of such devices and circuits under extreme temperatures. In this work, the performance of a high-speed gate driver with potential use in controlling power-level transistors was evaluated under extreme temperatures and thermal cycling. The investigations were carried out to assess performance for potential use of this device in space exploration missions under extreme temperature conditions.
    Keywords: Electronics and Electrical Engineering
    Type: GSFC-E-DAA-TN68254
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  • 3
    Publication Date: 2019-05-30
    Description: This release note discusses the planetary transit search data products produced by the Science Processing Operations Center at Ames Research Center from Sectors 1-2 observations made with the TESS (Transiting Exoplanet Survey Satellite) spacecraft and cameras as a means to document instrument performance and data characteristics.
    Keywords: Astronomy
    Type: NASA/TM-2019-220168 , ARC-E-DAA-TN65305
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  • 4
    Publication Date: 2019-05-21
    Description: In order to observe the lunar sodium exosphere out to one-half degree around the Moon, we designed, built and installed a small robotically controlled coronagraph at the Winer Observatory in Sonoita, Arizona. Observations are obtained remotely every available clear night from our home base at Goddard Space Flight Center or from Prescott, Arizona. We employ an Andover temperature-controlled 1.5-angstrom-wide narrow-band filter centered on the sodium D2 line, and a similar 1.5-angstrom filter centered blueward of the D2 line by 3 angstroms for continuum observations. Our data encompass lunations in 2015, 2016, and 2017, thus we have a long baseline of sodium exospheric calibrated images. During the course of three years we have refined the observational sequence in many respects. Therefore this paper only presents the results of the spring, 2017, observing season. We present limb profiles from the south pole to the north pole for many lunar phases. Our data do not fit any power of cosine model as a function of lunar phase or with latitude. The extended Na exosphere has a characteristic temperature of about 22506750 degrees Kelvin, indicative of a partially escaping exosphere. The hot escaping component may be indicative of a mixture of impact vaporization and a sputtered component.
    Keywords: Astronomy
    Type: GSFC-E-DAA-TN68105 , Icarus (ISSN 0019-1035) (e-ISSN 1090-2643); 328 ; 152-159
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  • 5
    Publication Date: 2019-05-22
    Description: An analysis was set up to model the temperature of the advanced modular power system (AMPS) power distribution cards when installed within the electronics enclosure case. The analysis was used to determine the steady-state temperature distribution of the cards within the case. To verify the analysis, an experiment was set up and conducted to simulate the operation of the cards within the enclosure. Four tests were conducted. The tests varied the position of the cold plate and evaluated the use of a thermal compound to reduce the contact resistance between the joints within the thermal path between the cards and the cold plate. Three of the four cases examined showed very good agreement between the analysis and the experiment with a less than 1-percent variation in the predicated temperatures determined through the analysis and the experimentally derived temperatures. In the remaining case, the difference between the analysis and experiment was approximately 12 percent. Both the experiment and analysis showed that the modular power conditioning cards can be maintained within their desired maximum operating temperature range of 40 to 45 C through thermal conduction to a cold plate when operating with their estimated maximum heat output of 16 W per card.
    Keywords: Electronics and Electrical Engineering
    Type: GRC-E-DAA-TN61712 , NASA/TM-2019-220011
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  • 6
    Publication Date: 2019-07-02
    Description: We present Zwicky Transient Facility (ZTF) observations of the tidal disruption flare AT2018zr/PS18kh reported by Holoien et al. and detected during ZTF commissioning. The ZTF light curve of the tidal disruption event (TDE) samples the rise-to-peak exceptionally well, with 50 days of g- and r-band detections before the time of maximum light. We also present our multi-wavelength follow-up observations, including the detection of a thermal (kT 100 eV) X-ray source that is two orders of magnitude fainter than the contemporaneous optical/UV blackbody luminosity, and a stringent upper limit to the radio emission. We use observations of 128 known active galactic nuclei (AGNs) to assess the quality of the ZTF astrometry, finding a median host-flare distance of 0farcs2 for genuine nuclear flares. Using ZTF observations of variability from known AGNs and supernovae we show how these sources can be separated from TDEs. A combination of light-curve shape, color, and location in the host galaxy can be used to select a clean TDE sample from multi-band optical surveys such as ZTF or the Large Synoptic Survey Telescope.
    Keywords: Astronomy
    Type: GSFC-E-DAA-TN67885 , Astrophysical Journal (ISSN 0004-637X) (e-ISSN 1538-4357); 872; 2; 198
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  • 7
    Publication Date: 2019-07-02
    Description: This release note discusses the science data products produced by the Science Processing Operations Center at Ames Research Center from the Sector 1-9 transiting planet search with observations made with the TESS spacecraft and cameras as a means to document instrument performance and data characteristics.
    Keywords: Astronomy
    Type: NASA/TM-2019–220228 , ARC-E-DAA-TN69032
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  • 8
    Publication Date: 2019-07-02
    Description: We present multiwavelength observations of the tidal disruption event (TDE) iPTF15af, discovered by the intermediate Palomar Transient Factory survey at redshift z = 0.07897. The optical and ultraviolet (UV) light curves of the transient show a slow decay over 5 months, in agreement with previous optically discovered TDEs. It also has a comparable blackbody peak luminosity of L(sub peak) approx. = 1.5 x 10(exp 44) erg s(exp -1). The inferred temperature from the optical and UV data shows a value of (35) 10(exp 4) K. The transient is not detected in X-rays up to L(sub X) 〈 3 x 10(exp 42) erg s(exp -1) within the first 5 months after discovery. The optical spectra exhibit two distinct broad emission lines in the He ii region, and at later times also H emission. Additionally, emission from [N iii] and [O iii] is detected, likely produced by the Bowen fluorescence effect. UV spectra reveal broad emission and absorption lines associated with high-ionization states of N v, C iv, Si iv, and possibly P v. These features, analogous to those of broad absorption line quasars (BAL QSOs), require an absorber with column densities N(sub H) 〉 10(exp 23) cm(exp -2). This optically thick gas would also explain the nondetection in soft X-rays. The profile of the absorption lines with the highest column density material at the largest velocity is opposite that of BAL QSOs. We suggest that radiation pressure generated by the TDE flare at early times could have provided the initial acceleration mechanism for this gas. Spectral UV line monitoring of future TDEs could test this proposal.
    Keywords: Astronomy
    Type: GSFC-E-DAA-TN67884 , Astrophysical Journal (ISSN 0004-637X) (e-ISSN 1538-4357); 873; 1; 92
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  • 9
    Publication Date: 2019-05-29
    Description: The first measurements of infrared (IR) band intensities of solid dimethyl carbonate are presented along with measurements of this compounds refractive index and density near 15 K, neither of which has been reported. Molar refractions are used to compare these results to other new data from ices made of methyl acetate, acetone, acetic acid, and acetaldehyde, four molecules known to exist in the interstellar medium. Comparisons are made to IR intensities taken from the literature on amorphous ices. The value and importance of comparisons based on molecular structures, to predict and test laboratory results, are highlighted.
    Keywords: Astronomy
    Type: GSFC-E-DAA-TN69110 , Physical Chemistry Chemical Physics (ISSN 1463-9076) (e-ISSN 1463-9084)
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  • 10
    Publication Date: 2019-06-27
    Description: We have adapted the algorithmic tools developed during the Kepler mission to vet the quality of transit-like signals for use on the K2 mission data. Using the four sets of publicly available light curves at MAST, we produced a uniformly vetted catalog of 772 transiting planet candidates from K2 as listed at the NASA Exoplanet Archive in the K2 Table of Candidates. Our analysis marks 676 of these as planet candidates and 96 as false positives. All confirmed planets pass our vetting tests. Sixty of our false positives are new identifications, effectively doubling the overall number of astrophysical signals mimicking planetary transits in K2 data. Most of the targets listed as false positives in our catalog show either prominent secondary eclipses, transit depths suggesting a stellar companion instead of a planet, or significant photocenter shifts during transit. We packaged our tools into the open-source, automated vetting pipeline Discovery and Vetting of Exoplanets (DAVE), designed to streamline follow-up efforts by reducing the time and resources wasted observing targets that are likely false positives. DAVE will also be a valuable tool for analyzing planet candidates from NASA's TESS mission, where several guest-investigator programs will provide independent light-curve setsand likely many more from the community. We are currently testing DAVE on recently released TESS planet candidates and will present our results in a follow-up paper.
    Keywords: Astronomy
    Type: GSFC-E-DAA-TN67861 , Astronomical Journal (ISSN 0004-6256) (e-ISSN 1538-3881); 157; 3; 124
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  • 11
    Publication Date: 2019-06-18
    Description: This release note discusses the planetary transit search data products produced by the Science Processing Operations Center at Ames Research Center from Sectors 1-6 observations made with the TESS (Transiting Exoplanet Survey Satellite) spacecraft and cameras as a means to document instrument performance and data characteristics.
    Keywords: Astronomy
    Type: NASA/TM-2019-220211 , ARC-E-DAA-TN68384
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  • 12
    Publication Date: 2019-06-19
    Description: Most violent and energetic processes in our universe, including mergers of compact objects,explosions of massive stars and extreme accretion events, produce copious amounts of X-rays. X-ray follow-up is an efficient tool for identifying transients: (1) X-rays can quickly localize transients with large error circles; (2) X-rays reveal the nature of transients that may not have unique signatures at other wavelengths. Here, we identify key science questions about several extragalactic multi-messenger andmulti-wavelength transients, and demonstrate how X-ray follow-up helps answer these questions.
    Keywords: Astronomy
    Type: GSFC-E-DAA-TN69843
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  • 13
    Publication Date: 2019-06-19
    Description: This presentation illustratively communicates how to SPICE model silicon carbide (SiC) SiC junction field effect transistors (JFETs) for designing circuits for NASA GRC's upcoming prototype fabrication of SiC JFET IC Version 12.
    Keywords: Electronics and Electrical Engineering
    Type: GRC-E-DAA-TN68630
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  • 14
    Publication Date: 2019-06-11
    Description: This presentation illustratively communicates integrated circuit (IC) mask design and layout rules for NASA GRC's upcoming prototype fabrication of SiC JFET IC Version 12.
    Keywords: Electronics and Electrical Engineering
    Type: GRC-E-DAA-TN68170
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  • 15
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    In:  CASI
    Publication Date: 2019-08-03
    Description: This presentation provides an overview of common mode conducted emissions (CMCE) measurements on power and signal cables. The presentation focuses on how such measurements directly apply to electromagnetic compatibility at the system level and provides a discussion of different techniques for performing them correctly and accurately.
    Keywords: Electronics and Electrical Engineering
    Type: GSFC-E-DAA-TN70541 , 2019 IEEE International Symposium on Electromagnetic Compatibility, Signal & Power Integrity; Jul 22, 2019 - Jul 26, 2019; New Orleans, LA; United States
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  • 16
    Publication Date: 2019-07-20
    Description: This release note discusses the science data products produced by the Science Processing Operations Center at Ames Research Center from Sector 3 observations made with the TESS spacecraft and cameras as a means to document instrument performance and data characteristics.
    Keywords: Astronomy
    Type: NASA/TM-2018-220181 , ARC-E-DAA-TN65303
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  • 17
    Publication Date: 2019-07-20
    Description: This release note discusses the planetary transit search data products produced by the Science Processing Operations Center at Ames Research Center from Sectors 1-3 observations made with the TESS spacecraft and cameras as a means to document instrument performance and data characteristics.
    Keywords: Astronomy
    Type: NASA/TM-2019-220180 , ARC-E-DAA-TN65309
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  • 18
    Publication Date: 2019-07-20
    Description: No abstract available
    Keywords: Astronomy
    Type: MSFC-E-DAA-TN66777 , MSFC-E-DAA-TN64113 , Meeting of the American Astronomical Society; Jan 06, 2019 - Jan 10, 2019; Seattle, WA; United States|Meeting of High Energy Astrophysics; Mar 17, 2019 - Mar 21, 2019; Monterey, CA; United States
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  • 19
    Publication Date: 2019-07-20
    Description: This release note discusses the science data products produced by the Science Processing Operations Center at Ames Research Center from Sector 7 observations made with the TESS spacecraft and cameras as a means to document instrument performance and data characteristics.
    Keywords: Astronomy
    Type: NASA/TM-2019-220170 , ARC-E-DAA-TN67170
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  • 20
    Publication Date: 2019-07-20
    Description: This release note discusses the science data products produced by the Science Processing Operations Center at Ames Research Center from Sector 8 observations made with the TESS spacecraft and cameras as a means to document instrument performance and data characteristics.
    Keywords: Astronomy
    Type: ARC-E-DAA-TN67719 , NASA/TM-2019-220191
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  • 21
    Publication Date: 2019-07-20
    Description: This release note discusses the science data products produced by the Science Processing Operations Center at Ames Research Center from Sector 4 observations made with the TESS spacecraft and cameras as a means to document instrument performance and data characteristics.
    Keywords: Astronomy
    Type: NASA/TM-2018-220167 , ARC-E-DAA-TN65304
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  • 22
    Publication Date: 2019-07-20
    Description: This release note discusses the science data products produced by the Science Processing Operations Center at Ames Research Center from Sector 6 observations made with the TESS spacecraft and cameras as a means to document instrument performance and data characteristics.
    Keywords: Astronomy
    Type: NASA/TM-2019-220166 , ARC-E-DAA-TN66263
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  • 23
    Publication Date: 2019-07-20
    Description: This release note discusses the science data products produced by the Science Processing Operations Center at Ames Research Center from Sector 5 observations made with the TESS spacecraft and cameras as a means to document instrument performance and data characteristics.
    Keywords: Astronomy
    Type: NASA/TM-2019-220048 , ARC-E-DAA-TN66262
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  • 24
    Publication Date: 2019-07-23
    Description: No abstract available
    Keywords: Electronics and Electrical Engineering
    Type: M19-7428 , NASA Electronic Parts and Packaging Electronic Technology Workshop; Jun 17, 2019 - Jun 20, 2019; Greenbelt, MD; United States
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  • 25
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    In:  CASI
    Publication Date: 2019-07-23
    Description: On 5 February 2015, a previously unknown meteor shower, the Lyrids were observed for the first time. Because of the Sun-Earth-Moon viewing geometry, however, stream members were observed almost exclusively by the Canadian Meteor Orbit Radar (CMOR). The Lyrids did not appear again until 2018, and that outburst was stronger than in 2015. This study analyzed the 2015 and 2018 CMOR data in order to determine the orbital parameters of the stream in an attempt to determine the Lyrid parent body. Of primary importance is to determine if the Lyrids will recur in a predictable manner. Two bodies, with dramatically different orbital parameters and evolutionary behaviors, emerged as the leading candidates: 2003 EH1 and 1854 R1.
    Keywords: Astronomy
    Type: M19-7356 , Meteoroids 2019; Jun 17, 2019 - Jun 21, 2019; Bratislava; Slovakia
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  • 26
    Publication Date: 2019-07-20
    Description: NASA Electronic Parts and Packaging (NEPP) Program Overview and Technology Highlights The NEPP Program provides NASA's leadership for developing and maintaining guidance for the screening, qualification, test, and reliable use of electrical, electronic, and electromechanical parts by NASA, in collaboration with other government agencies and industry. The NASA Electronic Parts Assurance Group (NEPAG) is a core portion of NEPP. This presentation highlights key focus areas for 2019.
    Keywords: Electronics and Electrical Engineering
    Type: GSFC-E-DAA-TN66532 , European Organization for Nuclear Research (CERN); Mar 19, 2019; Geneva; Switzerland
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  • 27
    Publication Date: 2019-07-20
    Description: This release note discusses the science data products produced by the Science Processing Operations Center at Ames Research Center from Sector 2 observations made with the TESS spacecraft and cameras as a means to document instrument performance and data characteristics.
    Keywords: Astronomy
    Type: NASA/TM-2018?220057 , ARC-E-DAA-TN64140
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  • 28
    Publication Date: 2019-07-20
    Description: Impact cratering is the dominant geo-logic process affecting the surfaces of solid bodies throughout our solar system. Because large impacts are (luckily) rare on Earth, the process is studied through experiments, observations of existing structures, numerical modeling, and theory, most of which make the simplifying assumptions that the target is homogeneous, with no substantial topography. Craters do not always form on level targets com-posed of homogeneous loose material. Rather (Fig. 1), they often form on sloped surfaces and in layered tar-gets, both of which significantly influence the excavation and ejecta deposition processes. Such craters are common on the Moon and asteroids. We are investigating crater formation in two separate suites of experiments using sloped and layered targets (Fig. 2) at the Experimental Impact Laboratory at NASA Johnson Space Center. An experiment was also performed in a flat, homogenous target to serve as a reference.
    Keywords: Astronomy
    Type: JSC-E-DAA-TN66691 , JSC-E-DAA-TN66690 , Lunar and Planetary Science Conference; Mar 18, 2019 - Mar 22, 2019; Woodlands, TX; United States
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  • 29
    Publication Date: 2019-07-20
    Description: The goal of this study was to perform an independent investigation of single event destructive and transient susceptibility of the Microsemi RTG4 device. The devices under test were the Microsemi RTG4 field programmable gate array (FPGA) Rev C. The devices under test will be referenced as the DUT or RTG4 Rev C throughout this document. The DUT was configured to have various test structures that are geared to measure specific potential susceptibilities of the device. DesignDevice susceptibility was determined by monitoring the DUT for Single Event Transient (SET) and Single Event Upset (SEU) induced faults by exposing the DUT to a heavy ion beam. Potential Single Event Latch-up (SEL) was checked throughout heavy-ion testing by monitoring device current.
    Keywords: Electronics and Electrical Engineering
    Type: GSFC-E-DAA-TN44754
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  • 30
    Publication Date: 2019-07-20
    Description: Microsemi (Microchip) RTG4 embedded triple modular redundant (TMR) phase-locked-loop (PLL) SEU data is presented. SEU data analysis includes: 1) Evaluation of heavy-ion beam angular effects (rectangular parallel pipe (RPP) or no RPP), 2) Importance of finding linear energy transfer (LET) onset (L0), 3) Comparison of prediction rate techniques.
    Keywords: Electronics and Electrical Engineering
    Type: GSFC-E-DAA-TN65147 , Microelectronics Reliability and Qualification Workshop (MRQW); Feb 05, 2019 - Feb 07, 2019; El Segundo, CA; United States
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  • 31
    Publication Date: 2019-07-25
    Description: No abstract available
    Keywords: Electronics and Electrical Engineering
    Type: M19-7451 , 2019 NASA Electronic Parts and Packaging Program (NEPP) Electronics Technology Workshop; Jun 17, 2019 - Jun 20, 2019; Greenbelt, MD; United States
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  • 32
    Publication Date: 2019-07-13
    Description: With the development of wide band-gap (WBG) technology, the switching speed of power semiconductor devices is increased, which makes circuits more sensitive to parasitics. For three-level active neutral point clamped (3L-ANPC) converters, the over-voltage of non-conducting switches can be an issue. This paper analyzes the multiple commutation loops in 3L-ANPC converter and summarizes the impact factors of the over-voltage for the non-conducting switch. It is found that the nonlinearity of the output capacitance of the device can significantly influence the over-voltage. A simple control without introducing any additional hardware circuit is proposed to attenuate the impact of the nonlinearity. With the proposed control, the peak over-voltage of the non-conducting switch can be reduced significantly. Multi-pulse test is conducted for a 3L- ANPC converter built with silicon carbide (SiC) MOSFETs. The testing results show that the peak over-voltage decreases from 892 V to 624 V with the proposed control. More detailed analysis and experimental results will be provided in the final paper.
    Keywords: Electronics and Electrical Engineering
    Type: GRC-E-DAA-TN68148 , IEEE COMPEL 2019; Jun 17, 2019 - Jun 20, 2019; Toronto; Canada
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  • 33
    Publication Date: 2019-07-13
    Description: This presentation illustratively communicates how to SPICE model integrated silicon carbide (SiC) SiC resistors for designing circuits for NASA GRC's upcoming prototype fabrication of SiC JFET IC Version 12.
    Keywords: Electronics and Electrical Engineering
    Type: GRC-E-DAA-TN68636 , HOTTech Microelectronics and Sensors Subgroup Monthly Meeting; May 24, 2019; Online
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  • 34
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    In:  CASI
    Publication Date: 2019-07-13
    Description: Nuclear fission power offers an attractive alternative to solar electric or radioisotope power systems for certain applications on the Moon, Mars, and deep space science missions. The advantages of independence from solar irradiance, high energy density, and abundance of fuel allow fission power systems to enable novel, high power mission architectures. While NASA has had numerous fission power programs throughout its history, few have gone far beyond the design phase. The recent test campaign called the Kilopower Reactor Using Stirling Technology project (KRUSTY) focused on a low power, kilowatt-scale design for simplicity and reduced cost, with the driving motivation to perform a full nuclear hardware prototype test. Following the successful completion of the KRUSTY nuclear hardware test in March of 2018, NASA has begun the formulation process for a Technology Demonstration Mission (TDM) using the Kilopower reactor technology. In support of NASA's lunar surface initiatives, the Kilopower TDM will target a 1-3 kW fission electric power system that can survive the lunar night and operate for one year. The system will be heavily influenced by the KRUSTY reactor design, using a solid Uranium metal core with high temperature heat pipes and Stirling engine power conversion. During this formulation phase, continued engineering efforts are ongoing to improve heat transfer efficiency in the system, examine fission radiation damage effects, and begin to address the thermal and structural requirements of a Kilopower flight system.
    Keywords: Electronics and Electrical Engineering
    Type: GRC-E-DAA-TN68456 , The Interagency Advanced Power Group (IAPG) Mechanical Working Group (MWG); May 14, 2019 - May 16, 2019; Houston, TX; United States
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  • 35
    Publication Date: 2019-07-13
    Description: No abstract available
    Keywords: Electronics and Electrical Engineering
    Type: M19-7326 , Annual CMSE Components for Military & Space Electronics Conference & Exhibition; Apr 16, 2019 - Apr 18, 2019; Los Angels, CA; United States
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  • 36
    Publication Date: 2019-07-13
    Description: NASA Electronic Parts and Packaging (NEPP) Program Overview Mission Statement: Provide NASA's leadership for developing and maintaining guidance for the screening, qualification, test, and reliable use of EEE parts by NASA, in collaboration with other government agencies and industry. The NASA Electronic Parts Assurance Group (NEPAG) is a core portion of NEPP.
    Keywords: Electronics and Electrical Engineering
    Type: GSFC-E-DAA-TN65660 , GSFC-E-DAA-TN65262 , GSFC-E-DAA-TN65146 , European Space Components Conference ESCCON 2019; Mar 11, 2019 - Mar 13, 2019; Noordwijk; Netherlands|2019 Space Parts Working Group (SPWG); Apr 30, 2019 - May 01, 2019; Torrance, CA; United States|Microelectronics Reliability and Qualification Workshop (MRQW); Feb 07, 2019; El Segundo, CA; United States
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  • 37
    Publication Date: 2019-08-02
    Description: The Laser Interferometer Space Antenna (LISA), requires high precision displacement measurement between widely spaced pairs of freely floating test masses. We describe a proposed design for the optical telescopes that form an essential part of the laser heterodyne interferometry measurement system and discuss how the design and implementation will address the unique challenges of this specialized application.
    Keywords: Astronomy
    Type: GSFC-E-DAA-TN71660 , Eduardo Amaldi Conference on Gravitational Waves; Jul 07, 2019 - Jul 12, 2019; Valencia; Spain|International Conference on General Relativity and Gravitation; Jul 07, 2019 - Jul 12, 2019; Valencia; Spain
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  • 38
    Publication Date: 2019-08-24
    Description: A multi-layer wireless sensor construct is provided. The construct includes a first dielectric layer adapted to be attached to a portion of a first surface of an electrically-conductive material. A layer of mu metal is provided on the first dielectric layer. A second dielectric layer is provided on the layer of mu metal. An electrical conductor is provided on the second dielectric layer wherein the second dielectric layer separates the electrical conductor from the layer of mu metal. The electrical conductor has first and second ends and is shaped to form an unconnected open-circuit that, in the presence of a time-varying magnetic field, resonates to generate a harmonic magnetic field response having a frequency, amplitude and bandwidth.
    Keywords: Electronics and Electrical Engineering
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  • 39
    Publication Date: 2019-08-13
    Description: The Icing Research Tunnel (IRT) at NASA Glenn Research Center follows the recommended practice for icing tunnel calibration outlined in SAE's ARP5905 document. The calibration team has followed the schedule of a full calibration every five years with a check calibration done every six months following. The liquid water content of the IRT has maintained stability within in the specifications presented to customers that the variation is within +/- 10% of the calibrated, target measurement. With recent measurements and instrumentation errors, a more thorough assessment of error source was desired. By constructing statistical process control charts, the ability to determine how the instrument varies in the short term, mid term, and long term was gained. The control charts offer a view of instrument error, facility error, or installation changes. It was discovered that there was a shift from target to mean baseline thus leading to the study of the overall capability indices of the liquid water content measuring instrument to perform within specifications defined in the IRT. This presentation describes data processing procedures for the Multi-Element Sensor in the IRT, including collision efficiency corrections, canonical correlation analysis, Chauvenet's Criterion for rejection of data, distribution check of data, and mean, median and mode for construction of control charts. Further data is presented to describe the repeatability of the IRT with the Multi-Element Sensor and the ability to maintain a stable process for the defined calibration schedule.
    Keywords: Electronics and Electrical Engineering
    Type: GRC-E-DAA-TN67428 , DATAWorks 2019 (Defense and Aerospace Test and Analysis Workshop); Apr 09, 2019 - Apr 11, 2019; Springfield, VA; United States
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  • 40
    Publication Date: 2019-08-13
    Description: ISO-26262, the road vehicle functional safety standard, underwent a major overhaul that was released in December 2018. Radiation effects, and single-event effect (SEE) hazards in particular, play an important role in autonomous vehicle safety. This connection will only increase as the level of driving automation goes from "hands off," to "eyes off," to "mind off." This translates to increased coupling with space climate and weather in addition to other traditional terrestrial radiation sources like thorium and uranium contamination in process and packaging materials. We will focus on autonomous vehicle radiation effects and present both benefits and challenges to the space weather and radiation engineering communities.
    Keywords: Electronics and Electrical Engineering
    Type: GSFC-E-DAA-TN68831 , Applied Space Environments Conference (ASEC 2019); May 13, 2019 - May 17, 2019; Los Angeles, CA; United States
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  • 41
    Publication Date: 2019-08-28
    Description: An integrated circuit (IC) chip with a self-contained fluid sensor and method of making the chip. The sensor is in a conduit formed between a semiconductor substrate and a non-conductive cap with fluid entry and exit points through the cap. The conduit may be entirely in the cap, in the substrate or in both. The conduit includes encased temperature sensors at both ends and a central encased heater. The temperature sensors may each include multiple encased diodes and the heater may include multiple encased resistors.
    Keywords: Electronics and Electrical Engineering
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  • 42
    Publication Date: 2019-08-28
    Description: A high-voltage power transmission system is used as an extremely large antenna to extract spatiotemporal space, physical, and geological information from geomagnetically induced currents (GIC). A differential magnetometer method is used to measure GIC and involves acquiring line measurements from a first fluxgate magnetometer under a high-voltage transmission line, acquiring natural field measurements from a reference magnetometer nearby but not under the transmission line, subtracting the natural field measurements from the line measurements, and determining the GIC-related Biot-Savart field from the difference. NASA warning and alarm systems can be triggered based on determinations of GIC amplitude levels that exceed a set threshold value.
    Keywords: Electronics and Electrical Engineering
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  • 43
    Publication Date: 2019-08-30
    Description: Increasing the power density and efficiency of electric machines (motors and generators) is integral to bringing Electrified Aircraft (EA) to commercial realization. To that end an effort to create a High Efficiency Megawatt Motor (HEMM) with a goal of exceeding 98% efficiency and 1.46 MW of power has been undertaken at the NASA Glenn Research Center. Of the motor components the resistive losses in the stator windings are by far the largest contributor (34%) to total motor loss. The challenge is the linear relationship between resistivity and temperature, making machine operation sensitive to temperature increases. In order to accurately predict the thermal behavior of the stator the thermal conductivity of the Litz wire-potting-electrical insulation system must be known. Unfortunately, this multi material system has a wide range of thermal conductivities (0.1 W/m-K 400 W/m-K) and a high anisotropy (axial vs transverse) making the prediction of the transverse thermal conductivity an in turn the hot spot temperatures in the windings is difficult. In order to do this a device that simulates the thermal environment found in the HEMM stator was designed. This device is not unlike the motorettes (little motors) that are described in IEEE standards for testing electrical insulation lifetimes or other electric motor testing. However, because the HEMM motor design includes significant rotor electrical and thermal considerations the term motorette was not deemed appropriate. Instead statorette (or little stator) was adopted as the term for this test device. This paper discussed the design, thermal heat conjugate analysis (thermal model), manufacturing and testing of HEMM's statorette. Analysis of the results is done by thermal resistance network model and micro thermal model and is compared to analytical predictions of thermal conductivity of the insulated and potted Litz wire system.
    Keywords: Electronics and Electrical Engineering
    Type: GRC-E-DAA-TN70196 , AIAA/IEEE Electric Aircraft Technologies Symposium (EATS); Aug 22, 2019 - Aug 24, 2019; Indianapolis, IN; United States
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  • 44
    Publication Date: 2019-08-30
    Description: X-ray observations are indispensable for understanding the cosmos. Their power is immense because much of the baryonic matter and the sites for the most active energy releases in the Universe are primarily observable in X-rays. For the 2030s and beyond, an X-ray observatory with power matching the capabilities in other wavebands is a necessary discovery engine for full exploration of the Universe. JWST and other upcoming major space- and ground-based facilities are expected to greatly expand science frontiers in the coming decades. is presents both a great opportunity and a challenge for a next-generation X-ray observatory. In many areas, such as tracing black holes during the CosmicDawn and understanding the formation and evolution of galaxies, an X-ray observatory is the logical next step. e challenge is that the X-ray science at these new frontiers requires expansion of capabilities by orders of magnitude beyond the current state of the art or anything already planned. Until recently, such gains were not technologically possible. is has changed thanks to recent breakthroughs and sustained maturation of key technologies for X-ray mirrors and detectors. We are reaping the fruits of U.S. investments in these areas over the past 1015 years. An X-ray observatory that can extend the science frontiers of the post-JWST era is now entirely feasible. Lynx is the mission concept that realizes this vision. It will y revolutionary optics and instrumentation onboard a simple, proven spacecraft. In all aspects, Lynx will be a next-generation Great Observatory that is certain to make a profound impact across the astrophysical landscape. It will provide the depth and breadth to answer the fundamental questions that confront us today; just as importantly, it will have capabilities to address questions we have yet to even ask.
    Keywords: Astronomy
    Type: MSFC-E-DAA-TN72489
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  • 45
    Publication Date: 2019-08-28
    Description: The Origins Space Telescope will trace the history of our origins from the time dust and heavy elements permanently altered the cosmic landscape to present-day life. How did galaxies evolve from the earliest galactic systems to those found in the universe today? How do habitable planets form? How common are life-bearing worlds? To answer these alluring questions, Origins will operate at mid- and far-infrared wavelengths and offer powerful spectroscopic instruments and sensitivity three orders of magnitude better than that of Herschel, the largest telescope flown in space to date. After a 3 year study, the Origins Science and Technology Definition Team will recommend to the Decadal Survey a concept for Origins with a 5.9-m diameter telescope cryo cooled to 4.5 K and equipped with three scientific instruments. A mid-infrared instrument (MISC-T) will measure the spectra of transiting exoplanets in the 2.8 20 m wavelength range and offer unprecedented sensitivity, enabling definitive biosignature detections. The Far-IR Imager Polarimeter (FIP) will be able to survey thousands of square degrees with broadband imaging at 50 and 250 m. The Origins Survey Spectrometer (OSS) will cover wavelengths from 25 588 m, make wide-area and deep spectroscopic surveys with spectral resolving power R ~ 300, and pointed observations at R ~ 40,000 and 300,000 with selectable instrument modes. Origins was designed to minimize complexity. The telescope has a Spitzer-like architecture and requires very few deployments after launch. The cryo-thermal system design leverages JWST technology and experience. A combination of current-state-of-the-art cryocoolers and next-generation detector technology will enable Origins natural background limited sensitivity.
    Keywords: Astronomy
    Type: GSFC-E-DAA-TN72131 , UV/Optical/IR Space Telescopes and Instruments: Innovative Technologies and Concepts; Aug 11, 2019 - Aug 12, 2019; San Diego, CA; United States
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  • 46
    Publication Date: 2019-11-02
    Description: The purpose of this document is to provide a forecast of major meteor shower activity in low Earth orbit (LEO). Typical activity levels are expected for nearly all showers in 2020; only the Geminids, which are gradually increasing in strength over time, are expected to be stronger than in previous years. No meteor storms or outbursts are predicted for 2020.
    Keywords: Astronomy
    Type: M19-7665
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  • 47
    Publication Date: 2019-10-31
    Description: Solar neutrons are the tell-tale of highly energetic processes (e.g. solar flares) at the Sun in which particle acceleration is taking place over a broad range in energy. Unlike charged radiation, neutrons escape unscathed from the ambient magnetic fields, providing a view of particle acceleration unhindered by the effects of transport. High-energy neutrons are challenging to measure with the traditional double scatter technique based on time-of-flight (ToF). This technique is limited by the finite flight path and active scintillator sizes required by small satellite platforms. The new SOlar Neutron TRACking (SONTRAC) concept, based on scintillating-fiber bundles, will provide high resolution imaging of fast neutrons at energies where the bulk of solar and magnetospheric neutrons resides. Recent development of the new SONTRAC instrument concept's advanced electronics and processing algorithms are presented.
    Keywords: Electronics and Electrical Engineering
    Type: GSFC-E-DAA-TN73731 , 2019 IEEE Nuclear Science Symposium (NSS) and Medical Imaging Conference (MIC); Oct 26, 2019 - Nov 02, 2019; Manchester; United Kingdom
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  • 48
    Publication Date: 2019-09-24
    Description: The Orbital Debris Program Office at NASA Johnson Space Center has a long history of an optical observational program. The Meter Class Autonomous Telescope, MCAT, was dedicated to Eugene Stansbery (now also known as ES-MCAT) in 2017. MCAT, a 1.3m DFM telescope, has a proven capability for tracking known objects from Low-Earth Orbits (LEO) out to Geosynchronous (GEO) orbits. Monitoring the population of the GEO belt is accomplished through surveys. A GEO survey statistically samples the GEO belt (0 to ~15 deg orbital inclinations) to detect both correlated and uncorrelated targets. A GEO survey, the initial focus for MCAT, will commence in 2019 to map out the current state of the GEO population as input for the ORbital Debris Engineering Model (ORDEM 4.x). If a break-up occurs, surveys of the break-up field can be followed for discovery and investigations of daughter debris fragments from the parent satellite. Discovery can be accomplished by surveying orbits near to and including the parent objects orbit. Targeted observations of debris can be taken with a suite of broadband filters for characterizing individual objects by rate-tracking their known or calculated orbital elements (Two-Line Element sets, TLEs). These observations can be used in conjunction with NASAs Standard Satellite Break-up Model (SSBM). In 2018, MCATs primary mirror was realuminized with a high-end protected, enhanced silver ZeCoat and the CCD chip was replaced in the Spectral Instruments camera. With these updates completed, MCAT is now well on track to reach Full Operational Capability (FOC) in 2019 for its survey and rate-track capabilities. A full overview of MCATs operational state, capabilities, and mission will be discussed.
    Keywords: Astronomy
    Type: JSC-E-DAA-TN67870 , Advanced Maui Optical and Space (AMOS) Surveillance Technologies Conference; Sep 17, 2019 - Sep 20, 2019; Maui, HI; United States
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  • 49
    facet.materialart.
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    In:  CASI
    Publication Date: 2019-10-25
    Description: This presentation highlights NASA AFRCs wireless systems development plans as well as technological needs and airworthiness challenges for flight test/research applications. The presentation discusses desired wireless sensing and wireless data communication methodologies for specific aircraft areas such as wings, tail, engines, and landing gears. The presentation also provides information for potential industry partners seeking to collaborate in the development of sensors through various means as well as to verify and validate wireless sensors and systems through flight at AFRC.
    Keywords: Electronics and Electrical Engineering
    Type: AFRC-E-DAA-TN73584 , Annual IEEE International Conference on Wireless for Space and Extreme Environments (WISEE 2019); Oct 16, 2019 - Oct 18, 2019; Ottawa; Canada
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  • 50
    Publication Date: 2019-10-08
    Description: Total ionizing dose (TID) and single-event effect (SEE) room-temperature radiation test results are presented for developmental prototype 4H-SiC junction field effect transistor (JFET) semiconductor integrated circuits (ICs) that have demonstrated prolonged operation in extremely high-temperature (500 C) environments. The devices tested demonstrated over 7 Mrad(Si) TID tolerance and no destructive SEE susceptibility.
    Keywords: Electronics and Electrical Engineering
    Type: GSFC-E-DAA-TN70540 , IEEE Nuclear and Space Radiation Effects Conference (NSREC); Jul 08, 2019 - Jul 12, 2019; San Antonio, TX; United States
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  • 51
    Publication Date: 2019-10-08
    Description: Total ionizing dose, displacement damage dose, and single-event effect testing were performed to characterize and determine the suitability of candidate electronics for NASA space utilization. Devices tested include optoelectronics, digital, analog, bipolar devices, and FPGAs.
    Keywords: Electronics and Electrical Engineering
    Type: GSFC-E-DAA-TN70538 , IEEE Nuclear and Space Radiation Effects Conference (NSREC); Jul 08, 2019 - Jul 12, 2019; San Antonio, TX; United States
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  • 52
    Publication Date: 2019-10-08
    Description: Total ionizing dose, displacement damage dose, and single-event effect testing were performed to characterize and determine the suitability of candidate electronics for NASA space utilization. Devices tested include optoelectronics, digital, analog, bipolar devices, and FPGAs.
    Keywords: Electronics and Electrical Engineering
    Type: GSFC-E-DAA-TN70510 , IEEE Nuclear and Space Radiation Effects Conference (NSREC); Jul 08, 2019 - Jul 12, 2019; San Antonio, TX; United States
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  • 53
    Publication Date: 2019-11-14
    Description: Outline -Introduction: Fermi Gamma-Ray Burst Monitor (GBM); Gamma-Ray Bursts (GRBs). -GRB 170817A: GBMs most famous GRB; Gamma-ray and Gravitational Wave (GW) Observations; Science from Joint GW/GRB observations; Timeline of follow-up observations. -Similar GRBs in GBM data: GRB 150101B; Other similar GRBs. -What comes next?: Joint GBM and LIGO (Laser Interferometer Gravitational-Wave Observatory) / Virgo (Michelson interferometer operated by a European consortium) observations; Science from new GW/GRB observations; New types of coincident events. -Other types of transient and variable sources observed with Fermi GBM.
    Keywords: Astronomy
    Type: MSFC-E-DAA-TN74876 , MSFC-E-DAA-TN67612 , Center for Relativistic Astrophysics (CRA) Seminar; Apr 18, 2019; Atlanta, GA; United States|Astronomy Presentation; Nov 07, 2019; New Haven, CT; United States
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  • 54
    Publication Date: 2019-11-09
    Description: Exoplanet science mission concepts require ultra-stable telescopes for multiple hours exposures. Predictive Thermal Control Study (PTCS) matures technology to enable active thermal controlled telescopes required to make ultra-high contrast observations of exoplanets. PTCS' goal is to develop an active thermal control technology that can keep mirrors at a constant temperature (〈 10 mK) regardless of where the telescope points on the sky.
    Keywords: Astronomy
    Type: MSFC-E-DAA-TN74859 , Annual Mirror Technology SBIR/STTR Workshop; Nov 05, 2019 - Nov 07, 2019; Redondo Beach, CA; United States
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  • 55
    Publication Date: 2019-11-09
    Description: No abstract available
    Keywords: Astronomy
    Type: MSFC-E-DAA-TN74849 , Annual Mirror Technology SBIR/STTR Workshop; Nov 05, 2019 - Nov 07, 2019; Redondo Beach, CA; United States
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  • 56
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    In:  CASI
    Publication Date: 2019-10-02
    Description: Single-Event Effects (SEE) testing was conducted on the nVidia Jetson TX2 System on Chip (SOC). Testing was conducted at Massachusetts General Hospital's (MGH) Francis H. Burr Proton Therapy Center on June 2nd, 2019.
    Keywords: Electronics and Electrical Engineering
    Type: GSFC-E-DAA-TN72754
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  • 57
    Publication Date: 2019-09-28
    Description: Comet C/2016 R2 (PanSTARRS) has a peculiar volatile composition, with CO being the dominant volatile, as opposed to H2O, and one of the largest N2/CO ratios ever observed in a comet. Using observations obtained with the Spitzer Space Telescope, NASAs Infrared Telescope Facility, the 3.5 m Astrophysical Research Consortium telescope at Apache Point Observatory, the Discovery Channel Telescope at Lowell Observatory, and the Arizona Radio Observatory 10 m Submillimeter Telescope, we quantified the abundances of 12 different species in the coma of R2 PanSTARRS: CO, CO2, H2O, CH4, C2H6, HCN, CH3OH, H2CO, OCS, C2H2, NH3, and N2. We confirm the high abundances of CO and N2 and heavy depletions of H2O, HCN, CH3OH, and H2CO compared to CO reported by previous studies. We provide the first measurements (or most sensitive measurements/constraints) on H2O, CO2, CH4, C2H6, OCS, C2H2, and NH3, all of which are depleted relative to CO by at least 12 orders of magnitude compared to values commonly observed in comets. The observed species also show strong enhancements relative to H2O, and, even when compared to other species like CH4 or CH3OH, most species show deviations from typical comets by at least a factor of 23. The only mixing ratios found to be close to typical are CH3OH/CO2 and CH3OH/CH4. The CO2/CO ratio is within a factor of 2 of those observed for C/1995 O1 (Hale- Bopp) and C/2006 W3 (Christensen) at a similar heliocentric distance, though it is at least an order of magnitude lower than many other comets observed with AKARI. While R2 PanSTARRS was located at a heliocentric distance of 2.8 au at the time of our observations in 2018 January/February, we argue, using sublimation models and comparison to other comets observed at similar heliocentric distance, that this alone cannot account for the peculiar observed composition of this comet and therefore must reflect its intrinsic composition. We discuss possible implications for this clear outlier in compositional studies of comets obtained to date and encourage future dynamical and chemical modeling in order to better understand what the composition of R2 PanSTARRS tells us about the early solar system.
    Keywords: Astronomy
    Type: GSFC-E-DAA-TN73044 , The Astronomical Journal (ISSN 0004-6256) (e-ISSN 1538-3881); 158; 3; 128
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  • 58
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    In:  Other Sources
    Publication Date: 2019-11-14
    Description: No abstract available
    Keywords: Astronomy
    Type: MSFC-E-DAA-TN74493 , Von Braun Astronomical Society (VBAS) Astronomy Day 2018; Oct 19, 2019; Huntsville, AL; United States
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  • 59
    Publication Date: 2019-08-08
    Description: Microprocessor, Graphics Processing Units (GPUs) and DDRx memory devices have emerged as promising next-generation technologies that enables both high performance processing and acceleration of complex algorithms for the latest challenges in human spaceflight, autonomous vehicles and artificial intelligence (AI). The feature sets of these devices offer exponential increases to throughput, calculation capability and system autonomy when compared to legacy flight systems. NASA's Electronic Part and Packaging (NEPP) Program has conducted an investigation into the radiation susceptibility of leading edge devices and process technologies by establishing standardized test approaches. Unlike most discrete devices, these require state of the art test systems to induce specific hardware activity similar to application software, thus allowing the characterization of failure modes within the system. To best characterize the tested part, NEPP eliminates variables that may impact device performance under radiation. Simplification of remaining system-level variables leads to an improved understanding of complex computational devices and their intended applications. The failure modes and error signatures that are recorded during testing are used to determine radiation sensitivity of the semiconductor process and the microcode architecture of the design. This presentation will discuss the test methodology that NASA Electronic Parts and Packaging (NEPP) is working to establish for its microprocessor, GPU and DDRx memory test programs to provide guidance on these devices and their underlying technology, in regards to their potential usage in future space flight systems.
    Keywords: Electronics and Electrical Engineering
    Type: GSFC-E-DAA-TN69964 , IEEE Space Computing Conference (SCC); Jul 30, 2019 - Aug 01, 2019; Pasadena, CA; United States
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  • 60
    Publication Date: 2020-01-23
    Description: Properly assessing the asteroid threat depends on the knowledge of asteroid pre-entry parameters, such as size, velocity, mass, density, and strength. Although a vast number of possible bodies to study exist, such characterization of asteroid populations is currently limited by substantial costs associated with space rendezvous missions and rare meteorite findings. As asteroids fragment, ablate, and decelerate in the atmosphere, they emit light detectable by ground-based and space-borne instruments. Earths atmosphere, thus, becomes an accessible laboratory that enables impactor risk assessments by facilitating inference of the pre-entry parameters. These asteroid pre-entry conditions are typically deduced by modeling the entry and breakup physics that best reproduce the observed light or energy deposition curve. However, this process requires extensive manual trial-and-error of uncertain modeling parameters. Automating meteor modeling and inference would improve property distributions used in risk assessments and enable population characterization as more light curves become more readily available through the presence of space assets and ground-based camera networks. We previously developed a genetic algorithm to automate meteor modeling by using the fragment-cloud model (FCM) to search for the values of the FCM input parameters (e.g., diameter) that generate energy deposition profiles that match the observed one. Now, we apply deep learning to infer asteroid diameter, velocity, and density from observed energy deposition curves. We trained and tested our neural network models with synthetic energy deposition curves modeled using the FCM rubble pile implementation. We present an application of a 1D convolutional neural network and compare its performance to other attempted regressors and machine learning techniques, such as a fully connected neural network and Random Forest regression, to demonstrate its capabilities. We validate our model weights and approach using the Chelyabinsk, Tagish Lake, Beneov, Koice, and Lost City meteors.
    Keywords: Astronomy
    Type: ARC-E-DAA-TN76511 , AGU Fall 2019 Meeting; Dec 09, 2019 - Dec 13, 2019; San Francisco, CA; United States
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  • 61
    Publication Date: 2020-01-23
    Description: Electromagnetic Compatibility (EMC) is essential to the success of any vehicle design that incorporates a complex assortment of electronic, electrical, and electromechanical systems and sub-systems that is expected to meet operational and performance requirements while exposed to a changing set of electromagnetic environments composed of both man-made and naturally occurring threats. The combined aspects of these environments are known as Electromagnetic Environmental Effects (E3). The attainment of EMC is accomplished through the application of sound engineering principles and practices that enable a complex vehicle or vehicles to operate successfully when exposed to the effects of its expected and/or specified electromagnetic environments.
    Keywords: Electronics and Electrical Engineering
    Type: DSG-RQMT-004 , JSC-E-DAA-TN72653-1
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  • 62
    Publication Date: 2020-01-18
    Description: High precision attitude measurement systems obviate the need for the beacon from the receiver making it possible for the spacecraft to beam a laser communications signal to a ground station without the ground station advertising its location. The research presented targets new detection and estimation methods to improve the accuracy in locating stars on a focal plane detector, and an understanding of the effects of changes in the optics design parameters and aberration, including defocus, on the navigation solution itself. This understanding can lead to an optimization of the attitude solution with respect to those optics realm parameter changes. The methodology discussed includes the development of a model of a current star tracker system. Using this model, multiple algorithms are implemented, including a multi-hypothesis method (MHT), to detect and estimate the position of the stars on the focal plane detector. It will be shown that using the MHT for detection and estimation, a greater accuracy can be found for each star estimation from more traditional detection and estimation algorithms. The approach then uses the model to develop statistics of the star tracker and the attitude estimation outputs to understand the accuracy, or variance, of the system's attitude solution. This solution is repeated for a range of defocus aberration, and a lower limit to the variance of the attitude solution is shown. A Cramer Rao lower bound solution is derived for the star tracker system and the results are compared to the Monte Carlo analysis from the model and shown to correlate very well. The approach uses a star image not as a Gaussian spot on the focal plane as done in previous work, and use of an image that includes the effects of aberrations of the optic system, and the effects of under-sampling and noise from the focal plane detector as well. Analysis includes exploring a star tracker's accuracy improvement through the combination of focus error and under-sampling effects alone, possibly contradicting conventional wisdom and approaches.
    Keywords: Electronics and Electrical Engineering
    Type: GRC-E-DAA-TN72340 , Advanced Maui Optical and Space Surveillance Technologies Conference (AMOS); Sep 17, 2019 - Sep 20, 2019; Maui, HI; United States
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  • 63
    Publication Date: 2019-08-27
    Description: Exoplanet Transmission Spectroscopy with LUVOIR
    Keywords: Astronomy
    Type: GSFC-E-DAA-TN72262 , Extreme Solar Systems IV; Aug 19, 2019 - Aug 23, 2019; Reykjavik; Iceland
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  • 64
    Publication Date: 2019-08-27
    Description: A series of electromagnetic simulations was conducted for the Conformal Lightweight Antenna System for Aeronautical Communications Technologies (CLAS-ACT) Program. The program designed, built, and flight tested a 14.25 GHz conformal patch array antenna for satellite communications on a T-34C airplane. Various studies were performed to evaluate the effects of antenna element spacing, array shape, signal taper, phased array pointing angle, null steering coefficients, antenna platform, and location on the airplane. This report documents the methods and some of the results of tests done over a 2 year period.
    Keywords: Electronics and Electrical Engineering
    Type: NASA/TM–2019-220293 , L-21041 , NF1676L-33695
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  • 65
    Publication Date: 2019-08-27
    Description: In Section 1 we summarize the technological approaches to the Large Balloon Reflector (LBR) that are discussed at length in our Phase I Technical report. Within each subsection we highlight how the work was advanced in Phase II. In Section 2 the work and lessons learned from the 3 and 5 meter LBR prototypes are described. In Section 3 the LBR Sensor Package stratospheric flight is described. Section 4 puts LBR in the context of on-going NASA missions.In Sections 5 and 6 the dissemination of results and plans to realize a stratospheric LBR are discussed. Instead of attempting to maintain the pointing of a large telescope at the end of a tether, we propose to deploy a telescope in the benign, protected environment within the carrier balloon. The telescope is itself a balloon, spherical in shape, metalized on one side and anchored to the top of the carrier balloon via a rotating azimuth plate (see Figure 2). The carrier balloon serves as both a stable mount and a radome for the inner balloon reflector. Light from space (or the atmosphere or ground) first passes through the ~2 mil thick polyethylene skin of the carrier balloon and then through the ~1 mil thickMylar side of the inner balloon. Together these layershave 〈 8% absorption at the wavelengths of interest.The incoming light then encounters the aluminized,spherical, back surface of the inner balloon and isthen focused into a receiving system. To achieve the performance of a 10 meter parabolic reflector, a 20 meter diameter inner balloon can be used with a modest size (~1 meter) spherical corrector.
    Keywords: Astronomy
    Type: HQ-E-DAA-TN65188
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  • 66
    Publication Date: 2019-07-16
    Description: Single-event effects and total ionizing dose testing is described for a 32-layer NAND flash memory, in both SLC and MLC configurations, with special considerations for unique three-dimensional test results.
    Keywords: Electronics and Electrical Engineering
    Type: GSFC-E-DAA-TN70578 , Nuclear and Space Radiation Effects Conference (NSREC); Jul 08, 2019 - Jul 12, 2019; San Antonio, TX; United States
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  • 67
    Publication Date: 2019-07-12
    Description: Short-period sub-Neptunes with substantial volatile envelopes are among the most common type of known exoplanets. However, recent studies of the Kepler population have suggested a dearth of sub-Neptunes on highly irradiated orbits, where they are vulnerable to atmospheric photoevaporation. Physically, we expect this "photoevaporation desert" to depend on the total lifetime X-ray and extreme ultraviolet flux, the main drivers of atmospheric escape. In this work, we study the demographics of sub-Neptunes as a function of lifetime exposure to high-energy radiation and host-star mass. We find that for a given present-day insolation, planets orbiting a 0.3 solar mass star experience approximately 100 times more X-ray flux over their lifetimes versus a 1.2 solar mass star. Defining the photoevaporation desert as a region consistent with zero occurrence at 2 sigma, the onset of the desert happens for integrated X-ray fluxes greater than 1.43 times 10 (sup 22) to 8.23 times 10 (sup 20) as a function of planetary radii for 1.8 to 4 Earth radius. We also compare the location of the photoevaporation desert for different stellar types. We find much greater variability in the desert onset in the bolometric flux space compared to the integrated X-ray flux space, suggestive of photoevaporation driven by steady-state stellar X-ray emissions as the dominant control on desert location. Finally, we report tentative evidence for the sub-Neptune valley, first seen around Sun-like stars, for M&K dwarfs. The discovery of additional planets around low-mass stars from surveys such as the Transiting Exoplanet Survey Satellite (TESS) mission will enable detailed exploration of these trends.
    Keywords: Astronomy
    Type: GSFC-E-DAA-TN69990 , The Astrophysical Journal (ISSN 2041-8205) (e-ISSN 2041-8213); 876; 1; 22
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  • 68
    Publication Date: 2019-12-11
    Description: Technology is changing at a fast pace. Transistor geometries are getting smaller, voltage thresholds are getting lower, design complexity is exponentially increasing, and user options are expanding. Consequently, reliable insertion of error detection and correction (EDAC) circuitry has become relatively challenging. As a response, a variety of mitigation techniques are being evaluated. They range from weak EDAC circuits that save area and power to strong mitigation strategies that are a great expense to systems. This presentation will focus on radiation induced susceptibilities for a variety of FPGA types and ASIC devices. In addition, the user will be provided information on applicable mitigation strategies per device.
    Keywords: Electronics and Electrical Engineering
    Type: GSFC-E-DAA-TN75288 , International School on the Effects of Radiation on Embedded Systems for Space Applications (SERESSA); Dec 02, 2019 - Dec 05, 2019; Seville; Spain
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  • 69
    Publication Date: 2019-11-08
    Description: Electrical power and control systems designed for use in planetary exploration missions and deep space probes require electronics that are capable of efficient and reliable operation under extreme temperature conditions. In addition, space-based infrared satellites, all-electric ships, jet engines, electromagnetic launchers, magnetic levitation transport systems, and power facilities are also typical examples where system electronics are expected to be exposed to harsh temperatures and to operate under severe thermal swings. Most commercial-off-the-shelf (COTS) devices are not designed to function under such extreme conditions and very little data exist on their performance outside their specified range of operation. In this work, the performance of an ultrafast gate driver for controlling power-level transistors was evaluated under extreme temperatures and thermal cycling. The investigations were carried out to assess performance for potential use of this device in space exploration missions under extreme temperature conditions.
    Keywords: Electronics and Electrical Engineering
    Type: GRC-E-DAA-TN73724
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  • 70
    Publication Date: 2019-11-05
    Description: The main goal of this project is to fulfill the need of a controller upgrade for the Cavity Environmental Control System (CECS) on the NASA SOFIA aircraft. The preceding controller had multiple disadvantages including operating in an unpressurized region, incomplete functionality implementation, limited fault and status monitoring capability, and reduced maintainability and reliability. The new controller will go through the NASA design process to fulfill all the requirements of CECS operation including complete functionality of all devices currently installed on the aircraft, added devices to improve fault and health monitoring, and overall improvement in maintainability and reliability.
    Keywords: Electronics and Electrical Engineering
    Type: AFRC-E-DAA-TN71278
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  • 71
    Publication Date: 2019-07-13
    Description: The analytical model for the device drain-source turn-on overvoltage in three-level active neutral point clamped (3L-ANPC) converters is established in this paper. Considering the two commutation loops in the converter, the relationship between the overvoltage and the loop inductances is evaluated. The line switching frequency device usually exhibits higher overvoltage, while the high switching frequency device is not strongly influenced by the multiple loops. A 500 kVA 3L-ANPC converter using SiC MOSFETs is tested, and the model is verified with the experimental results.
    Keywords: Electronics and Electrical Engineering
    Type: GRC-E-DAA-TN68909 , IEEE COMPEL 2019; Jun 17, 2019 - Jun 20, 2019; Toronto; Canada
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  • 72
    Publication Date: 2019-07-13
    Description: We have performed the initial characterization of single crystal 4H silicon carbide (4H-SiC) pressure sensors to determine the operational reliability over time at 800 C. Important parameters such as the zero pressure offset, bridge resistance, and pressure sensitivity as they are affected by temperature were extracted. These parameters showed relative stability within the prescribed operational envelop of the sensor at 800 C. Of significance is the increase in pressure sensitivity with increasing temperature beyond 400 C, to the extent that the sensitivity at 800 C was higher than the room temperature value. The implication of this result is that the sensor can be inserted further into the high temperature environment, thereby capturing the wider bandwidth of the pressure transients than currently possible.
    Keywords: Electronics and Electrical Engineering
    Type: GRC-E-DAA-TN67030 , International Conference on Solid State Sensors, Actuators and Microsystems: Transducers 2019; Jun 23, 2019 - Jun 27, 2019; Berlin; Germany
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  • 73
    Publication Date: 2019-07-13
    Description: Summary: GW170817 / GRB 170817A is one of the best observed transient and highlights the science impact of multi-messenger observations; Many open questions remain, with increased GW (Gravitational Wave) interferometer sensitivity, there will be more joint detections with GBM (Gamma-ray Burst Monitor), enabling deeper population studies of SGRBs (Short Gamma-Ray Bursts) -Additional distance measures which yield source energetics -Constrain jet structure and opening angle distribution -Cocoon emission from SGRBs -Causes of precursor and extended emission -Rates of SGRBs in the universe with implications for source evolution; Fermi GBM is currently the most prolific short GRB detector -Subthreshold searches are crucial to increasing GBM sensitivity and the detection horizon to weakevents like GRB 170817A; Looking forward to future multimessenger discoveries -Neutron star...Black hole merger, neutrinos, Fast Radio Bursts?
    Keywords: Astronomy
    Type: MSFC-E-DAA-TN65718 , University of Alabama Physics & Astronomy Colloquium; Feb 20, 2019; Tuscaloosa, AL; United States
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  • 74
    Publication Date: 2019-07-13
    Description: Mission success criteria at the device level and required device operation/availability can determine the risk posed by the radiation effects for a given device in a given environment, but rarely are the same from one mission to another. A large portion of New Space / SmallSat missions to date have benefitted from relatively short mission durations and chosen orbits that have less severe particle populations than their larger counterparts. As mission objectives grow and become reliant on their chosen devices operating for longer lives and in more harsh environments, requirements need to reflect the changing scope but not hinder design adoptions from previously successful missions that provide new capabilities. This presentation describes notable differences in radiation environments, the requirement changes that come with choice of orbit, and prioritizations for mission success criteria to be determined by the designers of the system and subsystems. Test methodologies based on radiation effect categories are explained briefly; when they are needed. Similarity data (and its limitations) are discussed so that caveats and short-comings are understood. Reliability and assurance quantification may not always be possible, but determining where risks are taken and how to classify them is the essential topic for the intended practice: to establish radiation requirements with the goal of getting to mission success.
    Keywords: Electronics and Electrical Engineering
    Type: GSFC-E-DAA-TN68975 , Single Event Effects (SEE) Symposium/Military and Aerospace Programmable Logic Devices (MAPLD) Workshop (SEE-MAPLD); May 20, 2019 - May 23, 2019; La Jolla, CA; United States
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  • 75
    Publication Date: 2019-07-13
    Description: NASA Glenn Research Center has been pursuing the development of dynamic power conversion for several decades. Candidate NASA missions involve mutli-year travel to far away destinations, or to extreme environments where sunlight does not exist. Human-base mission studies also show that power needs would be beyond the capabilities of solar energy conversion, and instead would require nuclear reactor energy sources, for which the thermal energy must be converted to electricity. Dynamic power conversion technology has developed sufficiently to make a sound engineering argument that it is suitable for these NASA missions. Dynamic conversion power sources have yet to be flown in space, and thus suffer a disadvantage owing to their lack of heritage data on flight missions. One of the largest obstacles for adoption is the uncertainty in reliability of a device with moving parts. However, significant progress has been made toward demonstrating the technology capable in all relevant environments, with the necessary long life. Another hurdle for adoption is the lack of mission, which would drive specific requirements, and provide a solid timeline for technology development endpoint. Until a mission is identified, an alternative approach is necessary to advance a dynamic power conversion system towards flight.
    Keywords: Electronics and Electrical Engineering
    Type: GRC-E-DAA-TN65656 , Nuclear and Emerging Technologies for Space; Feb 25, 2019 - Feb 28, 2019; Richland, WA; United States
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  • 76
    Publication Date: 2019-07-13
    Description: No abstract available
    Keywords: Electronics and Electrical Engineering
    Type: M19-7342 , NASA Breakthrough Materials Workshop; Apr 23, 2019 - Apr 24, 2019; Huntsville, AL; United States
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  • 77
    Publication Date: 2019-07-13
    Description: There are several mechanisms which have been proposed for the existence of colossal dielectric constant in the class of perovskite calcium copper titanate (CaCu3Ti4O12 or CCTO) materials. Researches indicate that existence of twinning parallel to (100) (001) and (010) planes causes planar defects and causes changes in local electronic structure. This change can cause insulating barriers locally which contribute to the large dielectric values irrespective of processing. The combination of insulating barriers, defects and displacements caused by twinning have been attributed to the generation of large dielectric constant in CCTO. To examine some of these arguments some researchers replaced Ca with other elements and evaluated this concept. In this study we present the synthesis and characterization of Ga2/3Cu3Ti4O12-xNx (GCTON) material. This provides both distortion due to atomic size difference and defects due to insertion of nitrogen. The morphology of the compound was determined to show that processing has tremendous effect on the dielectric values. The resistivity of GCTON was several order higher than CCTO and dielectric constant was higher than 10,000.
    Keywords: Electronics and Electrical Engineering
    Type: M19-7343 , SPIE Defense + Commercial Sensing; Apr 14, 2019 - Apr 18, 2019; Baltimore, MD; United States
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  • 78
    Publication Date: 2019-07-13
    Description: No abstract available
    Keywords: Electronics and Electrical Engineering
    Type: M19-7334 , NASAýs Breakthrough Materials Workshop; Apr 23, 2019 - Apr 24, 2019; Huntsville, AL; United States
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  • 79
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    In:  CASI
    Publication Date: 2019-07-13
    Description: The overall goal of this research project is to improve the response and sensitivity of the AC Retarding Potential Analyzer (RPA). The AC RPA can accurately measure the flux, energy, and energy distribution of charged particles in a space environment. The enhancement of the sensor derives from changes that increase sensitivity of flux measurements through reduction of the baseline noise. The enhanced AC RPA sensor allows diagnosis of required charge particle beams necessary for tests of materials, instruments and subsystems, for future exploration missions.
    Keywords: Electronics and Electrical Engineering
    Type: M19-7309 , STEM, LSAMP, HBCU-UP Joint Annual Conference; Apr 06, 2019; Tuskegee, AL; United States
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  • 80
    Publication Date: 2019-07-13
    Description: Overview of agency-level electronic parts management, the NASA Electronic Parts and Packaging (NEPP) Program, and NEPP Program Fiscal Year 2019 task investment areas.
    Keywords: Electronics and Electrical Engineering
    Type: GSFC-E-DAA-TN68250 , 2019 Space Parts Working Group (SPWG); Apr 30, 2019 - May 01, 2019; Torrance, CA; United States
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  • 81
    Publication Date: 2019-07-13
    Description: No abstract available
    Keywords: Electronics and Electrical Engineering
    Type: MSFC-E-DAA-TN67811 , 2019 Wearable Technologies Workshop; Apr 29, 2019 - Apr 30, 2019; Houston, TX; United States
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  • 82
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    In:  CASI
    Publication Date: 2019-07-13
    Description: In the 47 years since single-event effects were first observed in spacecraft electronics, radiation experts have developed an effective methodology supported by a nationwide infrastructure. A highly skilled workforce of radiation engineers has developed test facilities and methods, modeling and simulation techniques, and mitigation and design strategies to ensure space missions meet their performance and reliability requirements even in the harsh radiation environments of space. Now, increasing performance demands of space missions, the continued disruptive evolution of microcircuit technologies and growth and changes of the space industry have combined with an aging infrastructure are placing increasing strain on the radiation effects community, and the community is responding.
    Keywords: Electronics and Electrical Engineering
    Type: GSFC-E-DAA-TN67308 , Asilomar Microcomputer Workshop; Apr 24, 2019 - Apr 26, 2019; Pacific Grove, CA; United States
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  • 83
    Publication Date: 2019-07-13
    Description: We have performed a comprehensive spectral and timing analysis of the first NuSTAR observation of the high-mass X-ray binary 4U 1538522. The observation covers the X-ray eclipse of the source, plus the eclipse ingress and egress. We use the new measurement of the mid-eclipse time to update the orbital parameters of the system and find marginally significant evolution in the orbital period, with P(sub orb) / P(sub orb) = (-0.95 +/- 0.37) x 10(exp -6) yr(exp -1). The cyclotron line energy is found to be approximately 1.2 keV higher than RXTE measurements from 1997 to 2003, in line with the increased energy observed by Suzaku in 2012 and strengthening the case for secular evolution of 4U 1538522's CRSF. We additionally characterize the behavior of the iron fluorescence and emission lines and line-of-sight absorption as the source moves into and out of eclipse.
    Keywords: Astronomy
    Type: GSFC-E-DAA-TN66959 , Astrophysical Journal (ISSN 0004-637X) (e-ISSN 1538-4357); 873; 1; 62
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  • 84
    Publication Date: 2019-09-13
    Description: No abstract available
    Keywords: Astronomy
    Type: MSFC-E-DAA-TN72415 , Michigan Technological University Physics Colloquium; Sep 09, 2019; Houghton, MI; United States
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  • 85
    Publication Date: 2019-10-11
    Description: This paper introduces the new Portable Laser Guided Robotic antenna range (PLGR) at the National Aeronautics and Space Administration's (NASA) Glenn Research Center. Previous work used industrial robots in fixed facilities to characterize antennas and required fixtures that do not lend themselves to portable applications.NASA's PLGR system is designed for in-situ antenna measurements at a remote site. The system consists of a robot arm mounted on a vertical lift and a laser tracker, each on a portable base. The lift and laser tracker enable scanning a surface larger than the robot's reach. To accomplish this the robot first collects all points within its reach, then the system is moved and the laser tracker is used to relocate the robot before additional points are captured.The PLGR architecture will be discussed including how safety systems and path planning are combined to effectively characterize antennas. Software was written in high level languages for flexible integration of vector network analyzers and antenna controllers. Lastly, data will be shown to demonstrate the system functionality and accuracy.
    Keywords: Electronics and Electrical Engineering
    Type: GRC-E-DAA-TN71742 , AMTA 2019; Oct 06, 2019 - Oct 11, 2019; San Diego, CA; United States
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  • 86
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    In:  CASI
    Publication Date: 2019-10-02
    Description: Single-Event Effects (SEE) testing was conducted on the AMD e9173 Graphics Processor Unit (GPU). Testing was conducted at Massachusetts General Hospital's (MGH) Francis H. Burr Proton Therapy Center.
    Keywords: Electronics and Electrical Engineering
    Type: GSFC-E-DAA-TN72682
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  • 87
    Publication Date: 2019-10-02
    Description: Single-Event Effects (SEE) testing was conducted on the AMD Ryzen 3 2200G microprocessor with integrated graphics. Testing was conducted at Massachusetts General Hospital's (MGH) Francis H. Burr Proton Therapy Center on June 2nd, 2019.
    Keywords: Electronics and Electrical Engineering
    Type: GSFC-E-DAA-TN72756
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  • 88
    Publication Date: 2019-10-02
    Description: Single-Event Effects (SEE) testing was conducted on the AMD Ryzen 3 1200 microprocessor. Testing was conducted at Massachusetts General Hospital's (MGH) Francis H. Burr Proton Therapy Center on June 2nd, 2019.
    Keywords: Electronics and Electrical Engineering
    Type: GSFC-E-DAA-TN72755 , 2019-561-NEPP
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  • 89
    Publication Date: 2019-11-21
    Description: Gallium nitride (GaN), a wide bandgap (WBG) semiconductor, has emerged as a very promising material for electronic components due to the tremendous advantages it offers compared to silicon (Si), such as power capability, extreme temperature tolerance, and high frequency operation. This presentation summarizes a body of knowledge (BOK) document in reference to the development and current status of GaN technology obtained via literature and industry surveys. It provides a listing of the major manufacturers and their capabilities, as well as government, industry, and academic parties interested in the technology. The presentation also discusses GaN's applications in the area of power electronics, in particular those geared for space missions. Finally, issues relevant to the reliability of GaN-based electronic parts are addressed and limitations affecting the full utilization of this technology are identified.
    Keywords: Electronics and Electrical Engineering
    Type: GRC-E-DAA-TN70017 , NASA Electronic Parts and Packaging Program Electronics Technology Workshop; Jun 17, 2019 - Jun 20, 2019; Greenbelt, MD; United States
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  • 90
    Publication Date: 2019-11-13
    Description: Recent development in coating deposition processes for aluminum mirrors that are protected with a metal-fluoride overcoat (such as LiF, MgF2, or LiF) have improved reflectance.
    Keywords: Astronomy
    Type: GSFC-E-DAA-TN74948 , Annual Mirror Technology SBIR/STTR Workshop; Nov 05, 2019 - Nov 07, 2019; Redondo Beach, CA; United States
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  • 91
    Publication Date: 2020-01-17
    Description: This presentation describes an Intern experience working with analog to digital converters.
    Keywords: Electronics and Electrical Engineering
    Type: AFRC-E-DAA-TN76554
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  • 92
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    In:  CASI
    Publication Date: 2019-08-07
    Description: Reducing nonrecurring cost and shortening the build schedule for space qualified avionics has been a recurring theme in Space Industry. The NASA Goddard Space Flight Center has leverage its heritage flight qualified design and developed a portfolio of modular avionics comprised of 22 different board designs in a form factor named MUSTANG (Modular Unified Space Technology Avionics for Next Generation) that can be utilized in a variety flight applications. Since the design has no backplane, the modules can be mixed and match to meet the needed requirements. The MUSTANG form factor is sized to fill the void between 3U and 6U form factor and with flexibility to adapting the design without relaying out the boards.
    Keywords: Electronics and Electrical Engineering
    Type: GSFC-E-DAA-TN71223 , 2019 IEEE Space Computing Conference (SCC); Jul 30, 2019 - Aug 01, 2019; Pasadena, CA; United States
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  • 93
    Publication Date: 2019-12-10
    Description: The 1.3m ES-MCAT telescope (or MCAT for short) now has a proven capability for observing objects from Low- Earth Orbit (LEO) out to Geosynchronous (GEO) orbit, and the ability to run all systems autonomously. A GEO survey, the initial focus for MCAT, will commence in late 2019 to map out the current state of the GEO population as input for the ORbital Debris Engineering Model (ORDEM 4.x). This survey will statistically sample the GEO belt (0 to ~15 deg orbital inclinations) to detect both known and unknown targets. If a break-up occurs, additional surveys of the break-up field can be followed for discovery and investigations of daughter debris fragments from the parent satellite. Discovery can be accomplished by tracking orbits near to and including the parent objects orbit. Targeted observations of debris can be taken with a suite of broadband filters for characterizing individual objects by ratetracking their known or calculated orbital elements (Two-Line Element sets, TLEs). Several modifications and upgrades have been made to the instrumentation and systems originally installed in 2015 and are reported here. In 2018, MCATs primary mirror was recoated with a high-end protected, enhanced silver by the ZeCoat Corporation. The CCD chip was replaced in the Spectral Instruments camera with a broad-band antireflective coated chip. The automated weather systems have been modified from the original system, removing some weather sensors and installing replacements that are better suited to Ascensions weather and environment. A new 2.5-m ObservaDome replaced the Astrohaven dome on the nearby tower platform that will house an auxiliary 0.4-meter telescope. Finally, in 2019, the Observatory Control System was upgraded to 2.0 which includes additional flexibility for automating data collection and reduction. With these updates completed, MCAT is now well on track to reach Full Operational Capability (FOC) in 2019 for its survey, rate-track, and TLE tracking capabilities.
    Keywords: Astronomy
    Type: JSC-E-DAA-TN74105 , Advanced Maui Optical and Space Surveillance Technologies (AMOS) Conference; Sep 17, 2019 - Sep 20, 2019; Maui, HI; United States
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  • 94
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    American Association for the Advancement of Science (AAAS)
    In: Science
    Publication Date: 2018-08-03
    Keywords: Astronomy
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Geosciences , Computer Science , Medicine , Natural Sciences in General , Physics
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  • 95
    Publication Date: 2018-08-03
    Description: Tidal disruption events (TDEs) are transient flares produced when a star is ripped apart by the gravitational field of a supermassive black hole (SMBH). We have observed a transient source in the western nucleus of the merging galaxy pair Arp 299 that radiated 〉1.5 x 10 52 erg at infrared and radio wavelengths but was not luminous at optical or x-ray wavelengths. We interpret this as a TDE with much of its emission reradiated at infrared wavelengths by dust. Efficient reprocessing by dense gas and dust may explain the difference between theoretical predictions and observed luminosities of TDEs. The radio observations resolve an expanding and decelerating jet, probing the jet formation and evolution around a SMBH.
    Keywords: Astronomy
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Geosciences , Computer Science , Medicine , Natural Sciences in General , Physics
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  • 96
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    American Association for the Advancement of Science (AAAS)
    In: Science
    Publication Date: 2018-11-30
    Keywords: Astronomy
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Geosciences , Computer Science , Medicine , Natural Sciences in General , Physics
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  • 97
    Publication Date: 2018-11-30
    Description: Galaxy mergers and gas accretion from the cosmic web drove the growth of galaxies and their central black holes at early epochs. We report spectroscopic imaging of a multiple merger event in the most luminous known galaxy, WISE J224607.56–052634.9 (W2246–0526), a dust-obscured quasar at redshift 4.6, 1.3 billion years after the Big Bang. Far-infrared dust continuum observations show three galaxy companions around W2246–0526 with disturbed morphologies, connected by streams of dust likely produced by the dynamical interaction. The detection of tidal dusty bridges shows that W2246–0526 is accreting its neighbors, suggesting that merger activity may be a dominant mechanism through which the most luminous galaxies simultaneously obscure and feed their central supermassive black holes.
    Keywords: Astronomy
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Geosciences , Computer Science , Medicine , Natural Sciences in General , Physics
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  • 98
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    American Association for the Advancement of Science (AAAS)
    In: Science
    Publication Date: 2018-10-12
    Keywords: Astronomy
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Geosciences , Computer Science , Medicine , Natural Sciences in General , Physics
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  • 99
    Publication Date: 2018-10-12
    Description: Compact neutron star binary systems are produced from binary massive stars through stellar evolution involving up to two supernova explosions. The final stages in the formation of these systems have not been directly observed. We report the discovery of iPTF 14gqr (SN 2014ft), a type Ic supernova with a fast-evolving light curve indicating an extremely low ejecta mass (0.2 solar masses) and low kinetic energy (2 x 10 50 ergs). Early photometry and spectroscopy reveal evidence of shock cooling of an extended helium-rich envelope, likely ejected in an intense pre-explosion mass-loss episode of the progenitor. Taken together, we interpret iPTF 14gqr as evidence for ultra-stripped supernovae that form neutron stars in compact binary systems.
    Keywords: Astronomy
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Geosciences , Computer Science , Medicine , Natural Sciences in General , Physics
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  • 100
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    American Association for the Advancement of Science (AAAS)
    In: Science
    Publication Date: 2018-12-21
    Keywords: Astronomy
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Geosciences , Computer Science , Medicine , Natural Sciences in General , Physics
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