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    National Aeronautics and Space Administration

    EST. 1958
    3.1万论文总数
    128万引用总数

    The National Aeronautics and Space Administration (NASA /ˈnæsə/) is an independent agency of the U.S. federal government responsible for the civil space program, aeronautics research, and space research.[note 1]NASA was established in 1958, succeeding the National Advisory Committee for Aeronautics (NACA), to give the US space development effort a distinctly civilian orientation, emphasizing peaceful applications in space science. Since its establishment, most American space exploration efforts have been led by NASA, including the Apollo Moon landing missions, the Skylab space station, and later the Space Shuttle. NASA is supporting the International Space Station and is overseeing the development of the Orion spacecraft, the Space Launch System, Commercial Crew vehicles, and the planned Lunar Gateway space station. The agency is also responsible for the Launch Services Program, which provides oversight of launch operations and countdown management for uncrewed NASA launches.NASA's science is focused on better understanding Earth through the Earth Observing System; advancing heliophysics through the efforts of the Science Mission Directorate's Heliophysics Research Program; exploring bodies throughout the Solar System with advanced robotic spacecraft such as New Horizons; and researching astrophysics topics, such as the Big Bang, through the Great Observatories and associated programs.S.S.S.S.S.S.S.S.

    论文量&引用量时间轴

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    Glenn Diskin
    Glenn Diskin
    Langley Research Center, National Aeronautics and Space Administration
    论文:146引用:0H-index:0
    Martin Mlynczak
    Martin Mlynczak
    Christopher Newport University;Langley Research Center, National Aeronautics and Space Administration
    论文:137引用:0H-index:0
    Ron Noebe
    Ron Noebe
    National Aeronautics and Space Administration
    论文:111引用:0H-index:0
    Charles Bauschlicher
    Charles Bauschlicher
    Astrobiology Institute, National Aeronautics and Space Administration;Ames Research Center, National Aeronautics and Space Administration
    论文:110引用:0H-index:0
    Patrick Minnis
    Patrick Minnis
    Analytical Mechanics Associates, Inc.
    论文:107引用:0H-index:0
    James M. Russell III
    James M. Russell III
    Center for Atmospheric Sciences, Hampton University
    论文:90引用:0H-index:0
    David M. Winker
    David M. Winker
    Langley Research Center, National Aeronautics and Space Administration
    论文:78引用:0H-index:0
    Richard Ferrare
    Richard Ferrare
    NASA Langley Research Center
    论文:77引用:0H-index:0
    Timothy Lee
    Timothy Lee
    Space Sciences & Astrobiology Division, NASA Ames Research Center;NASA Astrobiology Institute
    论文:68引用:0H-index:0

    论文(10000)

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    1High Tide or Riptide on the Cosmic Shoreline? A Water-Rich Atmosphere or Stellar Contamination for the Warm Super-Earth GJ 486b from JWST Observations
    Sarah E. Moran,Kevin B. Stevenson,David K. Sing,Ryan J. Macdonald,James Kirk,Jacob Lustig-Yaeger,Sarah Peacock,L. C. Mayorga,Katherine A. Bennett,Mercedes Lopez-Morales,E. M. May,Zafar Rustamkulov,

    Planets orbiting M-dwarf stars are prime targets in the search for rocky exoplanet atmospheres. The small size of M dwarfs renders their planets exceptional targets for transmission spectroscopy, facilitating atmospheric characterization. However, it remains unknown whether their host stars' highly variable extreme-UV radiation environments allow atmospheres to persist. With JWST, we have begun to determine whether or not the most favorable rocky worlds orbiting M dwarfs have detectable atmospheres. Here, we present a 2.8-5.2 micron JWST NIRSpec/G395H transmission spectrum of the warm (700 K, 40.3x Earth's insolation) super-Earth GJ 486b (1.3 R$_{\oplus}$ and 3.0 M$_{\oplus}$). The measured spectrum from our two transits of GJ 486b deviates from a flat line at 2.2 - 3.3 $\sigma$, based on three independent reductions. Through a combination of forward and retrieval models, we determine that GJ 486b either has a water-rich atmosphere (with the most stringent constraint on the retrieved water abundance of H2O > 10% to 2$\sigma$) or the transmission spectrum is contaminated by water present in cool unocculted starspots. We also find that the measured stellar spectrum is best fit by a stellar model with cool starspots and hot faculae. While both retrieval scenarios provide equal quality fits ($\chi^2_\nu$ = 1.0) to our NIRSpec/G395H observations, shorter wavelength observations can break this degeneracy and reveal if GJ 486b sustains a water-rich atmosphere.

    2026ASTROPHYSICAL JOURNAL LETTERS(2026)引用:177
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    2Experimental Investigation and Analysis of Flow Condensation Heat Transfer in Microgravity-Experiments Onboard the International Space Station
    Issam Mudawar, Steven J. Darges,Mohammad M. Hasan,Henry K. Nahra, R. Balasubramaniam,Jeffrey R. Mackey

    This study presents the flow condensation heat transfer results of the Flow Boiling and Condensation Experiment (FBCE). The primary goal of FBCE is to obtain fundamental flow boiling and condensation heat transfer data in microgravity (mu ge) through experiments onboard the International Space Station. Experiments were performed with the Condensation Module for Heat Transfer (CM-HT), which is a tube-in-tube counterflow heat exchanger. Condensing nPFH flows through a stainless steel tube with an inner diameter of 7.24 mm and rejects heat to cooling water flowing in an annular channel (with inner and outer gap diameter of 7.94 and 12.70 mm, respectively) surrounding the tube. Experiments tested a broad range of nPFH mass velocities, G = 72.8 - 291.5 kg/m2s, inlet thermodynamic equilibrium qualities, xe,in = 0.28 - 1.19, inlet pressures, pin = 103.9 - 160.2 kPa, and water mass velocities, Gw = 129.4 - 324.7 kg/m2s. A parametric investigation shows local condensation heat transfer coefficient, h, is primarily dependent on G and local xe, which can be represented by the two-phase mixture Reynolds number, Retp. Channel averaged heat transfer coefficient in the saturated two-phase region, htp, increases with increasing G and xe,in. However, increasing inlet superheat does not affect htp, but does increase the heat transfer coefficient averaged over the entire channel, h. In the present experiments, G is sufficient to mitigate the effects of gravity, and htp in mu ge aligns with those for vertical down flow and horizontal flow in Earth gravity. Various correlations for htp were assessed, and the best performing correlation with a Mean Absolute Error (MAE) of 7.1% was that by Dorao and Fernandino, which is a function of Retp. Some correlations were shown to be overly dependent on the effect of gravity and were not applicable for the present mu ge database. A Separated Flow Model for annular condensation was employed to predict htp. The model's physical basis makes it seamlessly adaptable for mu ge, and it resulted in a MAE of 32.3%.

    2026INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER(2026)引用:4
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    3Leveraging High-Energy X-Ray Diffraction Microscopy and Crystal Plasticity Simulations to Study Grain Scale Stress Redistribution Within a Ti-7Al Sample Subjected to Creep
    Saikumar R. Yeratapally, Diwakar Naragani, Paul Shade,Armand Beaudoin, George Weber, Matthew Kasemer,Edward H. Glaessgen

    A series of far-field high-energy X-Ray diffraction microscopy (ff-HEDM) measurements gathered at discrete temporal points from the illuminated gage section of a Ti-7Al coupon subjected to creep revealed significant stress relaxation in soft grains neighboring a hard grain. A crystal plasticity finite element (CPFE) framework was used to perform a creep simulation on the tessellated volume of the gage section of the coupon based on the grain centroid data obtained from ff-HEDM. For a contiguous hard and soft grain pair, a correlation was found between grain-average stress relaxation (measured from experiments) and total accumulated slip (estimated from CPFE simulations). However, the magnitude of stress relaxation from CPFE simulation was significantly underpredicted due to the inherent homogeneous nature of the crystal plasticity framework which cannot resolve the mechanisms underpinning events (e.g., intermittent motion of dislocations, slip band formation, precipitate shearing, etc.) leading to stress relaxation in grains.

    2026SCRIPTA MATERIALIA(2026)引用:3
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    4Focused Laser Differential Interferometry: Recent Developments and Applications for Flow Measurements
    Elizabeth K. Benitez,Andrew Ceruzzi,Mark Gragston, Nicholaus J. Parziale,Bryan E. Schmidt,Joshua M. Weisberger
    2026AIAA Journal(2026)引用:3
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    5Spectral Mixture Modeling with Laboratory Near-Infrared Data I: Insights into Compositional Analysis of Europa
    A. Emran

    Europa's surface composition and physical characteristics are commonly constrained using spectral deconvolution through linear mixture (LM) modeling and radiative transfer-based (RT) intimate mixture modeling. Here, I compared the results of these two spectral modeling- LM versus RT- against laboratory spectra of water (H2O) ice and sulfuric acid octahydrate (SAO; H2SO48H(2)O) mixtures measured at near-infrared wavelengths (similar to 1.2-2.5 mu m) with grain sizes of 90-106 mu m (Hayes and Li, 2025). The modeled abundances indicate that the RT more closely reproduces the laboratory abundances, with deviations within +/- 5 % for both H2O ice and H2SO48H(2)O with similar to 100 mu m grains. In contrast, the LM shows slightly larger discrepancies, typically ranging from +/- 5-15 % from the true abundances. Interestingly, both LM and RT tend to consistently overestimate the abundance of H2SO48H(2)O and underestimate H2O ice across all mixtures. Nonetheless, when H2SO48H(2)O either dominates (>80 % as observed on Europa's trailing hemisphere; Carlson et al., 2005) or is present only in trace amounts (similar to 10 % on areas in Europa's leading hemisphere; Dalton et al., 2013; Ligier et al., 2016), both the LM and RT render acceptable results within +/- 10 % uncertainty. Thus, spectral modeling using the RT is preferred for constraining the surface composition across Europa, although the LM remains viable in specific compositional regimes.

    2026ICARUS(2026)引用:2
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