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  • Space Communications, Spacecraft Communications, Command and Tracking  (3)
  • Communications and Radar  (2)
  • 405; Center for Marine Environmental Sciences; Comment; DEPTH, sediment/rock; Gas chromatography; GC; GeoB13824-1; Gravity corer; M78/3A; MARUM; Meteor (1986); Methane  (1)
  • 498; Calcium carbonate; Carbon, organic, total; Center for Marine Environmental Sciences; DEPTH, sediment/rock; Element analyser, ELTRA; GC; GeoB13863-1; Gravity corer; M78/3B; MARUM; Meteor (1986)  (1)
  • 498; Center for Marine Environmental Sciences; DEPTH, sediment/rock; Element analyser, coupled to a DELTA V plus IRMS; GC; GeoB13863-1; Gravity corer; M78/3B; MARUM; Meteor (1986); δ34S, acid volatile sulfide; δ34S, chromium reducible sulfur; δ34S, elemental; δ34S, hydrogen sulfide; δ34S, sulfate; δ34S, total organic sulfur  (1)
  • Active Transport, Cell Nucleus  (1)
  • 2015-2019  (9)
  • 2016  (9)
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Keywords
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  • 2015-2019  (9)
Year
  • 2016  (9)
  • 1
    Publication Date: 2024-02-02
    Keywords: 405; Center for Marine Environmental Sciences; Comment; DEPTH, sediment/rock; Gas chromatography; GC; GeoB13824-1; Gravity corer; M78/3A; MARUM; Meteor (1986); Methane
    Type: Dataset
    Format: text/tab-separated-values, 42 data points
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  • 2
    Publication Date: 2024-02-02
    Keywords: 498; Calcium carbonate; Carbon, organic, total; Center for Marine Environmental Sciences; DEPTH, sediment/rock; Element analyser, ELTRA; GC; GeoB13863-1; Gravity corer; M78/3B; MARUM; Meteor (1986)
    Type: Dataset
    Format: text/tab-separated-values, 124 data points
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  • 3
    Publication Date: 2024-02-02
    Keywords: 498; Center for Marine Environmental Sciences; DEPTH, sediment/rock; Element analyser, coupled to a DELTA V plus IRMS; GC; GeoB13863-1; Gravity corer; M78/3B; MARUM; Meteor (1986); δ34S, acid volatile sulfide; δ34S, chromium reducible sulfur; δ34S, elemental; δ34S, hydrogen sulfide; δ34S, sulfate; δ34S, total organic sulfur
    Type: Dataset
    Format: text/tab-separated-values, 116 data points
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  • 4
    Publication Date: 2016-04-16
    Description: Nuclear pore complexes (NPCs) are 110-megadalton assemblies that mediate nucleocytoplasmic transport. NPCs are built from multiple copies of ~30 different nucleoporins, and understanding how these nucleoporins assemble into the NPC scaffold imposes a formidable challenge. Recently, it has been shown how the Y complex, a prominent NPC module, forms the outer rings of the nuclear pore. However, the organization of the inner ring has remained unknown until now. We used molecular modeling combined with cross-linking mass spectrometry and cryo-electron tomography to obtain a composite structure of the inner ring. This architectural map explains the vast majority of the electron density of the scaffold. We conclude that despite obvious differences in morphology and composition, the higher-order structure of the inner and outer rings is unexpectedly similar.〈br /〉〈span class="detail_caption"〉Notes: 〈/span〉Kosinski, Jan -- Mosalaganti, Shyamal -- von Appen, Alexander -- Teimer, Roman -- DiGuilio, Amanda L -- Wan, William -- Bui, Khanh Huy -- Hagen, Wim J H -- Briggs, John A G -- Glavy, Joseph S -- Hurt, Ed -- Beck, Martin -- 1R21AG047433-01/AG/NIA NIH HHS/ -- R21 AG047433/AG/NIA NIH HHS/ -- New York, N.Y. -- Science. 2016 Apr 15;352(6283):363-5. doi: 10.1126/science.aaf0643.〈br /〉〈span class="detail_caption"〉Author address: 〈/span〉Structural and Computational Biology Unit, European Molecular Biology Laboratory (EMBL), Heidelberg, Germany. ; Biochemistry Center of Heidelberg University, Im Neuenheimer Feld 328, D-69120 Heidelberg, Germany. ; Department of Chemistry, Chemical Biology and Biomedical Engineering, Stevens Institute of Technology, 507 River Street, Hoboken, NJ 07030, USA. ; Department of Anatomy and Cell Biology, McGill University, Montreal, Quebec, Canada. ; Structural and Computational Biology Unit, European Molecular Biology Laboratory (EMBL), Heidelberg, Germany. Cell Biology and Biophysics Unit, EMBL, Heidelberg, Germany.〈br /〉〈span class="detail_caption"〉Record origin:〈/span〉 〈a href="http://www.ncbi.nlm.nih.gov/pubmed/27081072" target="_blank"〉PubMed〈/a〉
    Keywords: Active Transport, Cell Nucleus ; Cryoelectron Microscopy ; Electron Microscope Tomography ; HeLa Cells ; Humans ; Mass Spectrometry ; Models, Molecular ; Nuclear Matrix/metabolism/ultrastructure ; Nuclear Pore/*metabolism/*ultrastructure ; Nuclear Pore Complex Proteins/chemistry/genetics/*metabolism
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Computer Science , Medicine , Natural Sciences in General , Physics
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  • 5
    Publication Date: 2019-07-13
    Description: We present performance data for novel photon-counting detectors for free space optical communication. NASA GSFC is testing the performance of two types of novel photon-counting detectors 1) a 2x8 mercury cadmium telluride (HgCdTe) avalanche array made by DRS Inc., and a 2) a commercial 2880-element silicon avalanche photodiode (APD) array. We present and compare dark count, photon-detection efficiency, wavelength response and communication performance data for these detectors. We successfully measured real-time communication performance using both the 2 detected-photon threshold and AND-gate coincidence methods. Use of these methods allows mitigation of dark count, after-pulsing and background noise effects. The HgCdTe APD array routinely demonstrated photon detection efficiencies of greater than 50% across 5 arrays, with one array reaching a maximum PDE of 70%. We performed high-resolution pixel-surface spot scans and measured the junction diameters of its diodes. We found that decreasing the junction diameter from 31 micrometers to 25 micrometers doubled the e- APD gain from 470 for an array produced in the year 2010 to a gain of 1100 on an array delivered to NASA GSFC recently. The mean single-photon SNR was over 12 and the excess noise factors measurements were 1.2-1.3. The commercial silicon APD array exhibited a fast output with rise times of 300 ps and pulse widths of 600 ps. On-chip individually filtered signals from the entire array were multiplexed onto a single fast output.
    Keywords: Communications and Radar
    Type: GSFC-E-DAA-TN29653 , SPIE Photonics West; Feb 13, 2016 - Feb 18, 2016; San Francisco, CA; United States
    Format: application/pdf
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  • 6
    Publication Date: 2019-07-13
    Description: We present performance data for novel photon counting detectors for free space optical communication. NASA GSFC is testing the performance of three novel photon counting detectors 1) a 2x8 mercury cadmium telluride avalanche array made by DRS Inc. 2) a commercial 2880 silicon avalanche photodiode array and 3) a prototype resonant cavity silicon avalanche photodiode array. We will present and compare dark count, photon detection efficiency, wavelength response and communication performance data for these detectors. We discuss system wavelength trades and architectures for optimizing overall communication link sensitivity, data rate and cost performance. The HgCdTe APD array has photon detection efficiencies of greater than 50 were routinely demonstrated across 5 arrays, with one array reaching a maximum PDE of 70. High resolution pixel-surface spot scans were performed and the junction diameters of the diodes were measured. The junction diameter was decreased from 31 m to 25 m resulting in a 2x increase in e-APD gain from 470 on the 2010 array to 1100 on the array delivered to NASA GSFC. Mean single photon SNRs of over 12 were demonstrated at excess noise factors of 1.2-1.3.The commercial silicon APD array has a fast output with rise times of 300ps and pulse widths of 600ps. Received and filtered signals from the entire array are multiplexed onto this single fast output. The prototype resonant cavity silicon APD array is being developed for use at 1 micron wavelength.
    Keywords: Space Communications, Spacecraft Communications, Command and Tracking
    Type: GSFC-E-DAA-TN29655 , SPIE Photonics West; Feb 13, 2016 - Feb 18, 2016; San Francisco, CA; United States|Free-Space Laser Communication and Atmospheric Propagation; Feb 15, 2016 - Feb 16, 2016; San Francisco, CA; United States
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  • 7
    Publication Date: 2019-12-24
    Description: In 2014, the Inter-agency Operations Advisory Group (IOAG) chartered a multi-agency team effort to study how to best handle spacecraft emergency as part of cross support among network assets. The original intent is to put in place for the first time a process and guidelines to make emergency support as part of a permanent cross-support capability between space agencies. From the perspective of space communications service providers, a few key issues, common to all agencies, concerning the Spacecraft Emergency Cross Support (SECS) have been explored. They are: context of emergency support, provision of emergency support under a cross-support agreement, provision of emergency support with no cross-support agreement, legal and liability issues, response time, support priority, services provided, sustaining emergency support capabilities, and charge for the support. The positions of the various participating agencies with respect to these issues have been collected, analyzed, and finally harmonized to form the recommended IOAG positions. A central challenge most communications service providers are facing is that since the spacecraft emergency is an unplanned critical event, it typically requires fast response to the emergency call, hence lacking an international standard process for the operational interfaces seems to exacerbate the difficulty in providing SECS. For reducing the response time, i.e. from the time of accepting a request for SECS to the readiness for support, it is recommended that a cross-support emergency system be established by IOAG member agencies. Along with it, the IOAG core services, just-in-time ground communications line, cross support service management (CSSM), and standard operations procedures (SOP) for operational interfaces form the basic foundation of the cross support emergency system. Of the above, new to the cross support conducted thus far in the IOAG community is the concept of the SOP specifically for the interfaces between the service provider and service user during the SECS. Use cases, salient features, and definition of the key operational activities/tasks relevant to the interfaces are addressed by the effort. Underpinning such a system is the availability of the RF license granted by the local authority, at national and/or regional level, for a given ground station to communicate with and track the spacecraft in emergency mode at the uplink and downlink frequencies assigned to that spacecraft. That means it is critical for the IOAG member agencies to obtain a priori all-band licenses (for the entire X-band or S-band) for some, if not all, of their ground stations that are most capable of or likely to provide SECS. It is also recommended that certain prior arrangements be made with the relevant local licensing authorities for a process that will allow expedited authorization to transmit/receive signals to/from the declared spacecraft over the declared ground stations specifically and solely for the emergency case. Our analysis of the SECS has also uncovered a few fundamental programmatic issues. Recognizing any IOAG positions reached on these issues do not necessarily lead to any binding authority, it is recommended that they, along with those key attributes of the cross support emergency system, be explicitly stated as multi-agency guidelines to guide the implementation and provision of the SECS. The paper will present the results of the working group on Spacecraft Emergency Cross Support and, in particular, its findings, products and recommendations. It will also identify the next steps of this work that may include the production of some international standards as an extension of this work, or the process to make this emergency system usable by other spacecraft operators beyond the space agencies.
    Keywords: Space Communications, Spacecraft Communications, Command and Tracking
    Type: AIAA 2016-2478 , JPL-CL-16-1996 , SpaceOps 2016 Conference; May 16, 2016 - May 20, 2016; Daejeon; Korea, Republic of
    Format: text
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  • 8
    Publication Date: 2019-07-13
    Description: Advanced Digital Beamforming (DBF) Synthetic Aperture Radar (SAR) technology is an area of research and development pursued at the NASA Goddard Space Flight Center (GSFC). Advanced SAR architectures enhances radar performance and opens a new set of capabilities in radar remote sensing. DBSAR-2 and EcoSAR are two state-of-the-art radar systems recently developed and tested. These new instruments employ multiple input-multiple output (MIMO) architectures characterized by multi-mode operation, software defined waveform generation, digital beamforming, and configurable radar parameters. The instruments have been developed to support several disciplines in Earth and Planetary sciences. This paper describes the radars advanced features and report on the latest SAR processing and calibration efforts.
    Keywords: Communications and Radar
    Type: GSFC-E-DAA-TN35269 , GSFC-E-DAA-TN36034 , 2016 IEEE International Symposium on Phased Array Systems and Technology; Oct 18, 2016 - Oct 21, 2016; Waltham, MA; United States
    Format: application/pdf
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  • 9
    Publication Date: 2019-12-24
    Description: In 2014, the Inter-agency Operations Advisory Group (IOAG) chartered a multi-agency team effort to study how to best handle spacecraft emergency as part of cross support among network assets. The original intent is to put in place for the first time a process and guidelines to make emergency support as part of a permanent cross-support capability between space agencies. From the perspective of space communications service providers, a few key issues, common to all agencies, concerning the Spacecraft Emergency Cross Support (SECS) have been explored. They are: context of emergency support, provision of emergency support under a cross-support agreement, provision of emergency support with no cross-support agreement, legal and liability issues, response time, support priority, services provided, sustaining emergency support capabilities, and charge for the support. The positions of the various participating agencies with respect to these issues have been collected, analyzed, and finally harmonized to form the recommended IOAG positions. A central challenge most communications service providers are facing is that since the spacecraft emergency is an unplanned critical event, it typically requires fast response to the emergency call, hence lacking an international standard process for the operational interfaces seems to exacerbate the difficulty in providing SECS. For reducing the response time, i.e. from the time of accepting a request for SECS to the readiness for support, it is recommended that a cross-support emergency system be established by IOAG member agencies. Along with it, the IOAG core services, just-in-time ground communications line, cross support service management (CSSM), and standard operations procedures (SOP) for operational interfaces form the basic foundation of the cross support emergency system. Of the above, new to the cross support conducted thus far in the IOAG community is the concept of the SOP specifically for the interfaces between the service provider and service user during the SECS. Use cases, salient features, and definition of the key operational activities/tasks relevant to the interfaces are addressed by the effort. Underpinning such a system is the availability of the RF license granted by the local authority, at national and/or regional level, for a given ground station to communicate with and track the spacecraft in emergency mode at the uplink and downlink frequencies assigned to that spacecraft. That means it is critical for the IOAG member agencies to obtain a priori all-band licenses (for the entire X-band or S-band) for some, if not all, of their ground stations that are most capable of or likely to provide SECS. It is also recommended that certain prior arrangements be made with the relevant local licensing authorities for a process that will allow expedited authorization to transmit/receive signals to/from the declared spacecraft over the declared ground stations specifically and solely for the emergency case. Our analysis of the SECS has also uncovered a few fundamental programmatic issues. Recognizing any IOAG positions reached on these issues do not necessarily lead to any binding authority, it is recommended that they, along with those key attributes of the cross support emergency system, be explicitly stated as multi-agency guidelines to guide the implementation and provision of the SECS. The paper will present the results of the working group on Spacecraft Emergency Cross Support and, in particular, its findings, products and recommendations. It will also identify the next steps of this work that may include the production of some international standards as an extension of this work, or the process to make this emergency system usable by other spacecraft operators beyond the space agencies.
    Keywords: Space Communications, Spacecraft Communications, Command and Tracking
    Type: AIAA 2016-2478 , JPL-CL-16-1306 , SpaceOps 2016 Conference; May 16, 2016 - May 20, 2016; Daejeon; Korea, Republic of
    Format: text
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