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  • Instrumentation and Photography  (21)
  • Astronomy  (7)
  • Man/System Technology and Life Support  (3)
  • 2010-2014  (18)
  • 2000-2004  (13)
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Year
  • 1
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    A Sample Return Container with Hermetic Seal (2000)
    In:  CASI
    Details
    Publication Date: 2004-12-03
    Description: A sample return container is being developed by Honeybee Robotics to receive samples from a derivative of the Champollion/ST4 Sample Acquisition and Transfer Mechanism or other samplers and then hermetically seal samples for a sample return mission. The container is enclosed in a phase change material (PCM) chamber to prevent phase change during return and re-entry to earth. This container is designed to operate passively with no motors and actuators. Using the sampler's featured drill tip for interfacing, transfer-ring and sealing samples, the container consumes no electrical power and therefore minimizes sample temperature change. The circular container houses a few isolated canisters, which will be sealed individually for samples acquired from different sites or depths. The drill based sampler indexes each canister to the sample transfer position, below the index interface for sample transfer. After sample transfer is completed, the sampler indexes a seal carrier, which lines up seals with the openings of the canisters. The sampler moves to the sealing interface and seals the sample canisters one by one. The sealing interface can be designed to work with C-seals, knife edge seals and cup seals. Again, the sampler provides all sealing actuation. This sample return container and co-engineered sample acquisition system are being developed by Honeybee Robotics in collaboration with the JPL Exploration Technology program.
    Keywords: Instrumentation and Photography
    Type: Concepts and Approaches for Mars Exploration; Part 1; 182-183; LPI-Contrib-1062-Pt-1
    Format: text
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    NASA TECHNICAL REPORTS
  • 2
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    Chandra Observations of Magnetic White Dwarfs and Their Theoretical Implications (2002)
    In:  Other Sources
    Details
    Publication Date: 2019-07-18
    Description: Observations of cool DA and DB white dwarfs have not yet been successful in detecting coronal X-ray emission but observations of late-type dwarfs and giants show that coronae are common for these stars. To produce coronal X-rays, a star must have dynamo-generated surface magnetic fields and a well-developed convection zone. There is strong observational evidence that the DA star LHS 1038 and the DB star GD 358 have weak and variable surface magnetic fields. Since these fields are likely to be generated by dynamo action and since both stars have well-developed convection zones, theory predicts detectable levels of coronal X-rays from these white dwarfs. However, we present analysis of Chandra observations of both stars showing no detectable X-ray emission. The derived upper limits for the X-ray fluxes provide strong constraints on theories of formation of coronae around magnetic white dwarfs.
    Keywords: Astronomy
    Format: text
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  • 3
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    Optical Characteristics of the Marshall Space Flight Center Solar Ultraviolet Magnetograph (2001)
    In:  Other Sources
    Details
    Publication Date: 2019-07-17
    Description: This paper will describe the scientific objectives of the MSFC SUMI project and the optical components that have been developed to meet those objectives. In order to test the scientific feasibility of measuring magnetic fields in the UV, a sounding rocket payload is being developed, This paper will describe the optical measurements that have been made on the SUMI telescope mirrors and polarization optics.
    Keywords: Instrumentation and Photography
    Type: UV/EUV and Visible Space Instrumentation for Astronomy and Solar Physics; Jul 29, 2001 - Aug 03, 2001; San Diego, CA; United States
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  • 4
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    Development of a Polarimeter for Magnetic Field Measurements in the Ultraviolet (2001)
    In:  Other Sources
    Details
    Publication Date: 2019-07-17
    Description: This paper will describe the polarizing optics that are being developed for an ultraviolet magnetograph (SUMI) which will be flown on a sounding rocket payload. With a limited observing program, the polarizing optics were optimized to make simultaneous observation at two magnetic lines CIV (155nm) and MgII (280). This paper will give a brief overview of the SUMI instrument, will describe the polarimeter that will be used in the sounding rocket program and will present some of the measurements that have been made on the (SUMI) polarization optics.
    Keywords: Instrumentation and Photography
    Type: Polarization Analysis and Measurement Analysis IV; Jul 29, 2001 - Aug 03, 2001; San Diego, CA; United States
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  • 5
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    The Marshall Space Flight Center Solar Utraviolet Magnetograph (2004)
    In:  Other Sources
    Details
    Publication Date: 2019-07-18
    Description: This paper will describe the objectives of the Marshall Space Flight Center (MSFC) Solar Ultraviolet Magnetograph Investigation (SUMI) and the optical components that have been developed to meet those objectives. In order to test the scientific feasibility of measuring magnetic fields in the W, a sounding rocket payload is being developed. This paper will discuss: (1) the scientific measurements that will be made by the SUMI sounding rocket program, (2) how the optics have been optimized for simultaneous measurements of two magnetic lines CIV (1550 Angstroms) and MgII (2800 Angstroms), and (3) the optical, reflectance, transmission and polarization measurements that have been made on the SUMI telescope mirrors and polarimeter.
    Keywords: Instrumentation and Photography
    Type: SPIE Astronomical Telescopes and Instrumentation 2004; Jun 21, 2004 - Jun 25, 2004; Glasgow, Scotland; United Kingdom
    Format: text
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  • 6
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    X-ray Spectrometer (2004)
    In:  Other Sources
    Details
    Publication Date: 2019-07-18
    Description: The X-ray Spectrometer (XRS) instrument is a revolutionary non-dispersive spectrometer that will form the basis for the Astro-E2 observatory to be launched in 2005. We have recently installed a flight spare X R S microcalorimeter spectrometer at the EBIT-I facility at LLNL replacing the XRS from the earlier Astro-E mission and providing twice the resolution. The X R S microcalorimeter is an x-ray detector that senses the heat deposited by the incident photon. It achieves a high energy resolution by operating at 0.06K and by carefully controlling the heat capacity and thermal conductance. The XRS/EBIT instrument has 32 pixels in a square geometry and achieves an energy resolution of 6 eV at 6 keV, with a bandpass from 0.1 to 12 keV (or more at higher operating temperature). The instrument allows detailed studies of the x-ray line emission of laboratory plasmas. The XRS/EBIT also provides an extensive calibration "library" for the Astro-E2 observatory.
    Keywords: Instrumentation and Photography
    Type: High Temperature Plasma Diagnostics 2004; Apr 18, 2004 - Apr 22, 2004; San Diego, CA; United States
    Format: text
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  • 7
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    NEA Multi-Chamber Sample Return Container with Hermetic Sealing (2000)
    In:  Other Sources
    Details
    Publication Date: 2019-07-17
    Description: A sample return container is being developed by Honeybee Robotics to receive samples from a derivative of the Champollion/ST4 Sample Acquisition and Transfer Mechanism or other samplers such as the 'Touch and Go' Surface Sampler (TGSS), and then hermetically seal the samples for a sample return mission. The container is enclosed in a phase change material (PCM) chamber to prevent phase change during return and re-entry to earth. This container is designed to operate passively with no motors and actuators. Using the rotation axis of the TGSS sampler for interfacing, transferring and sealing samples, the container consumes no electrical power and therefore minimizes sample temperature change. The circular container houses multiple isolated canisters, which will be sealed individually for samples acquired from different sites or depths. The TGSS based sampler indexes each canister to the sample transfer position, below the index interface for sample transfer. After sample transfer is completed, the sampler indexes a seal carrier, which lines up seals with the openings of the canisters. The sampler moves to the sealing interface and seals the sample canisters one by one. The sealing interface can be designed to work with C-seals, knife edge seals and cup seals. This sample return container is being developed by Honeybee Robotics in collaboration with the JPL Exploration Technology program. A breadboard system of the sample return container has been recently completed and tested. Additional information is contained in the original extended abstract.
    Keywords: Instrumentation and Photography
    Type: Near-Earth Asteroid Sample Return Workshop; 38-39; LPI-Contrib-1073
    Format: text
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  • 8
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    Prototyping a Global Soft X-Ray Imaging Instrument for Heliophysics, Planetary Science, and Astrophysics Science (2012)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: We describe current progress in the development of a prototype wide field-of-view soft X-ray imager that employs Lobstereye optics and targets heliophysics, planetary, and astrophysics science. The prototype will provide proof-of-concept for a future flight instrument capable of imaging the entire dayside magnetosheath from outside the magnetosphere. Such an instrument was proposed for the ESA AXIOM mission.
    Keywords: Astronomy
    Type: GSFC-E-DAA-TN9560 , Astronomische Nachrichten; 333; 4; 378-382
    Format: application/pdf
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  • 9
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    The High-Resolution X-Ray Microcalorimeter Spectrometer, SXS, on Astro-H (2012)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: The science and an overview of the Soft X-ray Spectrometer onboard the STRO-H mission are presented. The SXS consists of X-ray focusing mirrors and a microcalorimeter array and is developed by international collaboration lead by JAXA and NASA with European participation. The detector is a 6 x 6 format microcalorimeter array operated at a cryogenic temperature of 50 mK and covers a 3' x 3' field of view of the X-ray telescope of 5.6 m focal length. We expect an energy resolution better than 7 eV (FWHM, requirement) with a goal of 4 eV. The effective area of the instrument will be 225 square centimeters at 7 keV; by a factor of about two larger than that of the X-ray microcalorimeter on board Suzaku. One of the main scientific objectives of the SXS is to investigate turbulent and/or macroscopic motions of hot gas in clusters of galaxies.
    Keywords: Astronomy
    Type: GSFC.JA.7031.2012 , Journal of Low Temperature Physics; 167; 6-May; 795-802
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  • 10
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    Implications of Weak Link Effects on Thermal Characteristics of Transition-Edge Sensors (2012)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: Weak link behavior in transition-edge sensor (TES) microcalorimeters creates the need for a more careful characterization of a device's thermal characteristics through its transition. This is particularly true for small TESs where a small change in the bias current results in large changes in effective transition temperature. To correctly interpret measurements, especially complex impedance, it is crucial to know the temperature-dependent thermal conductance, G(T), and heat capacity, C(T), at each point through the transition. We present data illustrating these effects and discuss how we overcome the challenges that are present in accurately determining G and T from I-V curves. We also show how these weak link effects vary wi.th TES size. Additionally, we use this improVed understanding of G(T) to determine that, for these TES microcalorimeters. Kaptiza boundary resistance dominates the G of devices with absorbers while the electron-phonon coupling also needs to be considered when determining G for devices without absorbers
    Keywords: Instrumentation and Photography
    Type: GSFC.JA.7030.2012 , Journal of Low Temperature Physics; 167; 4-Mar; 121-128
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