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  • 1
    Publication Date: 2019-06-27
    Description: Space radiation hazards to Skylab project photographic film
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
    Type: NASA-CR-61329 , ER-10725
    Format: application/pdf
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  • 2
    Publication Date: 2021-07-03
    Description: The instrument package SEIS (Seismic Experiment for Internal Structure) with the three very broadband and three short‐period seismic sensors is installed on the surface on Mars as part of NASA's InSight Discovery mission. When compared to terrestrial installations, SEIS is deployed in a very harsh wind and temperature environment that leads to inevitable degradation of the quality of the recorded data. One ubiquitous artifact in the raw data is an abundance of transient one‐sided pulses often accompanied by high‐frequency spikes. These pulses, which we term “glitches”, can be modeled as the response of the instrument to a step in acceleration, while the spikes can be modeled as the response to a simultaneous step in displacement. We attribute the glitches primarily to SEIS‐internal stress relaxations caused by the large temperature variations to which the instrument is exposed during a Martian day. Only a small fraction of glitches correspond to a motion of the SEIS package as a whole caused by minuscule tilts of either the instrument or the ground. In this study, we focus on the analysis of the glitch+spike phenomenon and present how these signals can be automatically detected and removed from SEIS's raw data. As glitches affect many standard seismological analysis methods such as receiver functions, spectral decomposition and source inversions, we anticipate that studies of the Martian seismicity as well as studies of Mars' internal structure should benefit from deglitched seismic data.
    Description: Plain Language Summary: The instrument package SEIS (Seismic Experiment for Internal Structure) with two fully equipped seismometers is installed on the surface of Mars as part of NASA's InSight Discovery mission. When compared to terrestrial installations, SEIS is more exposed to wind and daily temperature changes that leads to inevitable degradation of the quality of the recorded data. One consequence is the occurrence of a specific type of transient noise that we term “glitch”. Glitches show up in the recorded data as one‐sided pulses and have strong implications for the typical seismic data analysis. Glitches can be understood as step‐like changes in the acceleration sensed by the seismometers. We attribute them primarily to SEIS‐internal stress relaxations caused by the large temperature variations to which the instrument is exposed during a Martian day. Only a small fraction of glitches correspond to a motion of the whole SEIS instrument. In this study, we focus on the detection and removal of glitches and anticipate that studies of the Martian seismicity as well as studies of Mars's internal structure should benefit from deglitched seismic data.
    Description: Key Points: Glitches due to steps in acceleration significantly complicate seismic records on Mars. Glitches are mostly due to relaxations of thermal stresses and instrument tilt. We provide a toolbox to automatically detect and remove glitches.
    Description: Centre National d'Etudes Spatiales (CNES)
    Description: InSight PSP Program
    Description: Agence Nationale de la Recherche http://dx.doi.org/10.13039/501100001665
    Description: ANR‐19‐CE31‐0008‐08
    Keywords: 523 ; InSight ; seismometer ; Mars ; data processing ; glitches ; removal
    Type: article
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  • 3
    Publication Date: 2021-07-21
    Description: The densely farmed U.S. Midwest is a prominent source of nitrous oxide (N2O) but top‐down and bottom‐up N2O emission estimates differ significantly. We quantify Midwest N2O emissions by combining observations from the Atmospheric Carbon and Transport‐America campaign with model simulations to scale the Emissions Database for Global Atmospheric Research (EDGAR). In October 2017, we scaled agricultural EDGAR v4.3.2 and v5.0 emissions by factors of 6.3 and 3.5, respectively, resulting in 0.42 nmol m−2 s−1 Midwest N2O emissions. In June/July 2019, a period when extreme flooding was occurring in the Midwest, agricultural scaling factors were 11.4 (v4.3.2) and 9.9 (v5.0), resulting in 1.06 nmol m−2 s−1 Midwest emissions. Uncertainties are on the order of 50 %. Agricultural emissions estimated with the process‐based model DayCent (Daily version of the CENTURY ecosystem model) were larger than in EDGAR but still substantially smaller than our estimates. The complexity of N2O emissions demands further studies to fully characterize Midwest emissions.
    Description: Plain Language Summary: Nitrous oxide (N2O) is the third most important anthropogenic greenhouse gas contributing to the warming of the planet and the dominant man‐made ozone‐depleting substance in the stratosphere. Its atmospheric concentrations have been rising since industrialization mainly due to an increase in anthropogenic sources, with agriculture being the dominant source. The densely farmed U.S. Midwest plays an important role in the global N2O budget. However, previous studies that have collected observations of N2O indicate that estimates of surface emissions in the Midwest are substantially underestimating the truth. In this study, we combine unique aircraft‐based N2O measurements and model simulations to quantify Midwest emissions in October 2017 and June/July 2019. Agricultural inventory estimates had to be increased by factors up to 20 to match observations, revealing a large underestimation in current inventories. An extreme flooding event in 2019 when the summer observations occurred may be responsible for some of this discrepancy. Estimations of soil N2O emissions calculated with a state‐of‐the‐art biogeochemical model show less underestimation but are still too low compared to the fluxes derived from the aircraft observational data.
    Description: Key Points: Within the ACT‐America project, we gathered a unique airborne in‐situ N2O data set over the U.S. Midwest with enhancements up to 9  ppb. N2O emissions in the U.S. Midwest were on average 0.42 ± 0.28 nmol m−2 s−1 in October 2017 and 1.06 ± 0.57 nmol m−2 s−1 in June to July 2019. Bottom‐up estimates from EDGAR and DayCent underestimate U.S. Midwest N2O emissions by factors up to 20.
    Keywords: agriculture ; climate change ; flux estimate ; Midwest ; nitrous oxide ; top‐down
    Type: article
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  • 4
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    John Wiley and Sons, 550 pp.
    In:  New York, John Wiley and Sons, 550 pp., vol. 2, no. 3, pp. 2-203, (ISBN 0-521-59067-1 hc (0-521-59933-4 pb))
    Publication Date: 1973
    Keywords: Statistical investigations
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  • 5
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    In:  Pageoph, London, Army Corps of Engineers, Woodward-Clyde Consultants, vol. 112, no. B12, pp. 811-818, pp. 1013, (ISBN: 0-12-018847-3)
    Publication Date: 1974
    Keywords: Geomagnetics ; Induced seismicity ; Tectonics
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  • 6
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    In:  Tectonophys., London, Army Corps of Engineers, Woodward-Clyde Consultants, vol. 22, no. B12, pp. 363-375, pp. 1013, (ISBN: 0-12-018847-3)
    Publication Date: 1974
    Keywords: Elasticity theory of dislocations ; Dislocation ; Volcanology ; Crustal deformation (cf. Earthquake precursor: deformation or strain) ; StressS
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  • 7
    Publication Date: 2005-11-27
    Description: Sonic boom in near field and far field of nonlifting rectangular wing
    Keywords: AIRCRAFT
    Type: 3D CONF. ON SONIC BOOM RES. 1971; P 219-226
    Format: text
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  • 8
    Publication Date: 2005-11-27
    Description: Sonic boom cusped shock wave near focusing ray system of supersonic wing flow field
    Keywords: AIRCRAFT
    Type: 3D CONF. ON SONIC BOOM RES. 1971; P 133-146
    Format: text
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  • 9
    Publication Date: 2005-11-27
    Description: Flow field approximation for sonic boom shock wave generation by thin nonlifting rectangular wing
    Keywords: AIRCRAFT
    Type: 3D CONF. ON SONIC BOOM RES. 1971; P 123-132
    Format: text
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  • 10
    Publication Date: 2005-11-30
    Description: The development of weight-saving advanced design concepts for shuttle airframe structure is presented. Design concepts under investigation employ selective composite reinforcement and/or efficient geometric arrangements. An effort to develop metallic panel designs which exploit the relaxation of smooth external-surface requirements for skin structure is reviewed. Available highlights from research and development studies which investigate the application of composite reinforcement to the design of two types of fuselage panels, a shear web, a large fuselage frame, and a landing-gear-door assembly are presented. Preliminary results from these studies suggest weight savings of 25 percent can be obtained.
    Keywords: SPACE VEHICLES
    Type: NASA Space Shuttle Technol. Conf.; p 537-572
    Format: text
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