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  • Other Sources  (54)
  • 2015-2019  (54)
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  • 1
    Publication Date: 2019-07-13
    Description: The dual-wall, Whipple shield is the shield of choice for lightweight, long-duration flight. The shield uses an initial sacrificial wall to initiate fragmentation and melt an impacting threat that expands over a void before hitting a subsequent shield wall of a critical component. The key parameters to this type of shield are the rear wall and its mass which stops the debris, as well as the minimum shock wave strength generated by the threat particle impact of the sacrificial wall and the amount of room that is available for expansion. Ensuring the shock wave strength is sufficiently high to achieve large scale fragmentation/melt of the threat particle enables the expansion of the threat and reduces the momentum flux of the debris on the rear wall. Three key factors in the shock wave strength achieved are the thickness of the sacrificial wall relative to the characteristic dimension of the impacting particle, the density and material cohesion contrast of the sacrificial wall relative to the threat particle and the impact speed. The mass of the rear wall and the sacrificial wall are desirable to minimize for launch costs making it important to have an understanding of the effects of density contrast and impact speed. An analytic model is developed here, to describe the influence of these three key factors. In addition this paper develops a description of a fourth key parameter related to fragmentation and its role in establishing the onset of projectile expansion.
    Keywords: Spacecraft Design, Testing and Performance
    Type: JSC-CN-32626 , Hypervelocity Impact Symposium; Apr 26, 2015 - Apr 30, 2015; Boulder, CO; United States
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  • 2
    Publication Date: 2019-07-13
    Description: Fused silica window systems are used heavily on crewed reentry vehicles, and they are currently being used on the next generation of US crewed spacecraft, Orion. These systems improve crew situational awareness and comfort, as well as, insulating the reentry critical components of a spacecraft against the intense thermal environments of atmospheric reentry. Additionally, these materials are highly exposed to space environment hazards like solid particle impacts. This paper discusses impact studies up to 10 km/s on a fused silica window system proposed for the Orion spacecraft. A ballistic limit equation that describes the threshold of perforation of a fuse silica pane over a broad range of impact velocities, obliquities and projectile materials is discussed here.
    Keywords: Space Transportation and Safety
    Type: JSC-CN-32614 , Hypervelocity Impact Symposium; Apr 26, 2015 - Apr 30, 2015; Boulder, CO; United States
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  • 3
    Publication Date: 2019-07-13
    Description: No abstract available
    Keywords: Documentation and Information Science; Meteorology and Climatology
    Type: MSFC-E-DAA-TN37811 , AGU Fall Meeting; Dec 12, 2016 - Dec 16, 2016; San Francisco, CA; United States
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  • 4
    Publication Date: 2019-07-20
    Description: No abstract available
    Keywords: Documentation and Information Science
    Type: MSFC-E-DAA-TN67461 , EGU General Assembly; Apr 07, 2019 - Apr 12, 2019; Vienna; Austria
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  • 5
    Publication Date: 2019-07-13
    Description: No abstract available
    Keywords: Space Sciences (General)
    Type: JSC-E-DAA-TN68134 , Interagency Debris Coordination Meeting; May 07, 2019 - May 10, 2019; Rome; Italy
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  • 6
    Publication Date: 2019-07-13
    Description: No abstract available
    Keywords: Documentation and Information Science
    Type: MSFC-E-DAA-TN53560 , EGU General Assembly 2018; Apr 08, 2018 - Apr 13, 2018; Vienna; Austria
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  • 7
    Publication Date: 2019-07-13
    Description: We report the detection of coherent pulsations from the ultraluminous X-ray source (ULX) NGC 7793P13. The approx. =0.42 s nearly sinusoidal pulsations were initially discovered in broadband X-ray observations using XMM-Newton and NuSTAR taken in 2016. We subsequently also found pulsations in archival XMM-Newton data taken in 2013 and 2014. The significant (〉〉5(sigma)) detection of coherent pulsations demonstrates that the compact object in P13 is a neutron star, and given the observed peak luminosity of 10(exp 40) erg/ s (assuming isotropy), it is well above the Eddington limit for a 1.4 Stellar Mass accretor. This makes P13 the second ULX known to be powered by an accreting neutron star. The pulse period varies between epochs, with a slow but persistent spin-up over the 2013-2016 period. This spin-up indicates a magnetic field of B1.51012 G, typical of many Galactic accreting pulsars. The most likely explanation for the extreme luminosity is a high degree of beaming; however, this is difficult to reconcile with the sinusoidal pulse profile.
    Keywords: Astrophysics
    Type: GSFC-E-DAA-TN46807 , The Astrophysical Journal Letters (ISSN 2041-8205) (e-ISSN 2041-8213); 831; 2; L14
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  • 8
    Publication Date: 2019-07-13
    Description: Numerous mission support hardware systems and their spares are maintained outside of the habitable volume of the International Space Station (ISS), and are arranged covered by a multi-layer insulation (MLI) thermal blanket which provides both thermal control and a measure of protection from micrometeoroids and orbital debris (MMOD). The NASA Hypervelocity Impact Technology (HVIT) group at the Johnson Space Center in Houston Texas has assessed the protection provided by MLI in a series of hypervelocity impact tests using a 1 mm thick aluminum 6061-T6 rear wall to simulate the actual hardware behind the MLI. HVIT has also evaluated methods to enhance the protection provided by MLI thermal blankets. The impact study used both aluminum and steel spherical projectiles accelerated to speeds of 7 km/s using a 4.3 mm, two-stage, light-gas gun at the NASA White Sands Test Facility (WSTF).
    Keywords: Spacecraft Design, Testing and Performance
    Type: JSC-CN-35651-3 , Meeting of the Inter-Agency Debris Coordination Committee; Mar 29, 2016 - Apr 01, 2016; Didcot; United Kingdom
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  • 9
    Publication Date: 2019-07-13
    Description: We present results from four new broadband X-ray observations of the extreme ultraluminous X-ray source Holmberg IX X-1 (L (sub X) greater than 10 (sup 40) ergs per second), performed by Suzaku and NuSTAR in coordination. Combined with the archival data, we now have broadband observations of this remarkable source from six separate epochs. Two of these new observations probe lower fluxes than seen previously, allowing us to extend our knowledge of the broadband spectral variability exhibited. The spectra are well fit by two thermal blackbody components that dominate the emission below 10 kiloelectronvolts, as well as a steep (Gamma approximately equal to 3.5) power-law tail thatdominates above approximately 15 kiloelectronvolts. Remarkably, while the 0.3-10.0 kiloelectronvolts flux varies by a factor of approximately 3 between all these epochs, the 15-40 kiloelectronvolts flux varies by only approximately 20 percent. Although the spectral variability is strongest in the approximately 1-10 kiloelectronvolts band, both of the thermal components are required to vary when all epochs are considered. We also revisit the search for iron absorption features by leveraging the high-energy NuSTAR data to improve our sensitivity to extreme velocity outflows in light of the ultra-fast outflow recently detected in NGC 1313 X-1. Iron absorption from a similar outflow along our line of sight can be ruled out in this case. We discuss these results in the context of super-Eddington accretion models that invoke a funnel-like geometry for the inner flow, and propose a scenario in which we have an almost face-on view of a funnel that expands to larger radii with increasing flux, resulting in an increasing degree of geometrical collimation for the emission from intermediate-temperature regions.
    Keywords: Astrophysics
    Type: GSFC-E-DAA-TN46238 , Astrophysical Journal (ISSN 2041-8205) (e-ISSN 2041-8213); 839; 2; 105
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  • 10
    Publication Date: 2019-07-13
    Description: We present Neutron Star Interior Composition Explorer (NICER) observations of the neutron star (NS) low-mass X-ray binary Serpens X-1 during the early mission phase in 2017. With the high spectral sensitivity and low-energy X-ray passband of NICER, we are able to detect the Fe L line complex in addition to the signature broad, asymmetric Fe K line. We confirm the presence of these lines by comparing the NICER data to archival observations with XMM-Newton/Reflection Grating Spectrometer (RGS) and NuSTAR. Both features originate close to the innermost stable circular orbit (ISCO). When modeling the lines with the relativistic line model RELLINE, we find that the Fe L blend requires an inner disk radius of 1.4(sup 0.2, sub -0.1)R(sub ISCO) and Fe K is at 1.03(sup 0.13, sub -0.03)R(sub ISCO) (errors quoted at 90%). This corresponds to a position of 17(sup 2.5, sub -1.2)km and 12(sup 1.6, sub -0.4)km for a canonical NS mass (M(sub NS)=1.4 solar mass) and dimensionless spin value of a = 0. Additionally, we employ a new version of the RELXILL model tailored for NS(sub s) and determine that these features arise from a dense disk and supersolar Fe abundance.
    Keywords: Astrophysics
    Type: GSFC-E-DAA-TN57931 , The Astrophysical Journal Letters (ISSN 2041-8205) (e-ISSN 2041-8213); 858; L5; No. 1
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