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nasa
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Image
Published: 01 December 2004
Fig. 52 TRW-NASA VI A, as-cast. Blocky, light constituent is primary γ′; the black spots are carbide particles; the mottled gray areas are precipitated γ′ in a matrix of γ solid solution. Electrolytic etch: H 2 SO 4 and methanol. Original magnification 250×
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Published: 01 January 2000
Fig. 4 NASA five-ball RCF testing apparatus. (See Table 1 .) Source: Ref 22
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Published: 01 January 2001
Fig. 1 Construction of Boeing 737/NASA composite spoiler. Length, 130 cm (52 in.); width, 56 cm (22 in.); surface area, 1.5 m 2 (15.8 ft 2 ); weight, 5 kg (12 lb)
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Published: 31 December 2017
Fig. 2 National Aeronautics and Space Administration (NASA) five-ball rolling-contact fatigue testing apparatus. See Table 1 .
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in Modeling of Residual Stress and Machining Distortion in Aerospace Components
> Metals Process Simulation
Published: 01 November 2010
Fig. 27 Good agreement between DEFORM predictions (solid lines) and NASA's measurements (dotted lines) of the axial distortions of disk 1 after heat treatment and after two machining cuts
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Book: Casting
Series: ASM Handbook
Volume: 15
Publisher: ASM International
Published: 01 December 2008
DOI: 10.31399/asm.hb.v15.a0005228
EISBN: 978-1-62708-187-0
... discusses various microgravity solidification experiments that involve pure metals, alloys, and semiconductors and presents the official NASA acronyms for them. MEPHISTO, TEMPUS, the isothermal dendritic growth experiment, and advanced gradient heating facility, are also discussed. crystal growth...
Abstract
Gravity has profound influences on most solidification and crystal growth processes. Modification of gravity over practical time scales for the purposes of modifying or controlling solidification proves to be a far more daunting and expensive technological challenge. This article discusses various microgravity solidification experiments that involve pure metals, alloys, and semiconductors and presents the official NASA acronyms for them. MEPHISTO, TEMPUS, the isothermal dendritic growth experiment, and advanced gradient heating facility, are also discussed.
Series: ASM Handbook
Volume: 1
Publisher: ASM International
Published: 01 January 1990
DOI: 10.31399/asm.hb.v01.a0001052
EISBN: 978-1-62708-161-0
... of the NASA Conservation of Strategic Aerospace Materials (COSAM) program. advanced processing concepts alternate materials COSAM program gas turbine engines strategic materials strategic element substitution superalloys US reserves THE SUPERALLOYS are critical to the economic survival...
Abstract
This article reviews some of the trends in superalloy development as they relate to U.S. strategic materials availability and the aerospace industry. It discusses the supply sources and availability of strategic materials and summarizes the status of U.S. resources and reserves. The article presents a list of several superalloys that have been used in gas turbine engines or that are emerging as replacements because of the promise of increased operating temperatures and higher efficiencies for the aircraft of the future. It concentrates on the objectives, results, and methodology of the NASA Conservation of Strategic Aerospace Materials (COSAM) program.
Book Chapter
Book: Fractography
Series: ASM Handbook
Volume: 12
Publisher: ASM International
Published: 01 January 1987
DOI: 10.31399/asm.hb.v12.a0000631
EISBN: 978-1-62708-181-8
... ( Fig. 1326 ) was converted to an oxide of silver ( Fig. 1327 ). Both reflectivity and electrical conductivity decreased as a result. SEM, 3800× (R.J. Schwinghamer, NASA Marshall Space Flight Center) Fig. 1326 Fig. 1327 Fig. 1328, 1329 Integrated circuit (IC) defects. Material: pure...
Abstract
This article is an atlas of fractographs that helps in understanding the causes and mechanisms of fracture of electronic materials, including L-shaped electronic flat pack, transistor base lead, ohmic contact window, and brush/slip ring assembly. The fractographs illustrate the atomic oxygen environment exposure effect, solar cell interconnect, integrated circuit defects, and fatigue failure of these materials.
Book: Thermal Spray Technology
Series: ASM Handbook
Volume: 5A
Publisher: ASM International
Published: 01 August 2013
DOI: 10.31399/asm.hb.v05a.a0005733
EISBN: 978-1-62708-171-9
.... Department of Energy , p 419 – 437 , www.netl.doe.gov/technologies/coalpower/turbines/refshelf/handbook/4.4.2.pdf (accessed June 15, 2012) 6. Stecura S. , “Effects of Compositional Changes on the Performance of a Thermal Barrier Coating System,” NASA TM-78976, National Aeronautics and Space...
Abstract
This article presents a summary of the current and new materials and processing techniques for thermal barrier coatings (TBCs) and environmental barrier coatings (EBCs). Different thermal spraying and postspraying processing techniques are required to produce coatings with optimal performance. For TBCs and EBCs, the elastic modulus, mechanical strength, and toughness values are extremely important in predicting failure behavior under stress and strain conditions, mainly for modeling purposes. Sand and/or volcanic ash particles are molten in the hot zones of turbines and deposited over TBCs and EBCs. They form calcium-magnesium-aluminosilicate (CMAS) glassy deposits.
Book Chapter
Book: Corrosion: Materials
Series: ASM Handbook
Volume: 13B
Publisher: ASM International
Published: 01 January 2005
DOI: 10.31399/asm.hb.v13b.a0003842
EISBN: 978-1-62708-183-2
Abstract
This article examines the high-temperature oxidation of silica-forming ceramics under constant temperature and cyclic conditions. The effects of water vapor, impurities, and molten salts are discussed. The article describes the oxidation and corrosion of silica-forming composites, oxide ceramics, non-silica forming nitrides, carbides, and borides. The performance of environmental barrier coatings by material type is also discussed. The article also explains the effects of oxidation and corrosion on the mechanical properties of ceramic-matrix composites. It concludes with information on high-temperature applications, wear properties, and the microscopic analyses of advanced ceramics.
Book: Composites
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003430
EISBN: 978-1-62708-195-5
... that is deemed to be proprietary. There is, for example, extensive work on machining, joining, and coating of C-C composites for various military applications, which could be accessed by those with the appropriate clearances and need to know. The National Aeronautic and Space Administration (NASA) programs...
Abstract
Post-processing includes various processes that might be required to produce finished components from the ceramic-matrix composites (CMC) materials. The processes consist of machining or finishing operations, coating, joining, assembly operations, and nondestructive evaluation of CMCs and its components. This article discusses the specific needs for science and technology in these areas relative to the goal of employing CMCs in a variety of applications.
Series: ASM Handbook
Volume: 11
Publisher: ASM International
Published: 15 January 2021
DOI: 10.31399/asm.hb.v11.a0006758
EISBN: 978-1-62708-295-2
Abstract
The goal of using nondestructive evaluation (NDE) in conjunction with failure analysis is to obtain the most comprehensive set of data in order to characterize the details of the damage and determine the factors that allowed the damage to occur. The NDE results can be used to determine optimal areas upon which to focus for sectioning and metallography in order to further investigate the condition of the component. This article provides information on the inspection method available for failure analysis, including standard methods such as visual testing, penetrant testing, and magnetic particle testing. It covers the effects of various factors on the properties of the part that may impact failure analysis, describes the characterization of damage modes and crack sizes, and finally discusses the processes involved in application of NDE results to failure analysis.
Series: ASM Handbook
Volume: 11
Publisher: ASM International
Published: 15 January 2021
DOI: 10.31399/asm.hb.v11.a0006759
EISBN: 978-1-62708-295-2
... analyzer taking readings in situ. (a) Example of a handheld device. (b) Interface between the sample and the detector. Courtesy of J. Sampson, NASA Portable arc or spark optical emission spectrometers allow for in situ chemical analysis of suspect parts in a quantitative manner, with the possibility...
Abstract
Chemical analysis is a critical part of any failure investigation. With the right planning and proper analytical equipment, a myriad of information can be obtained from a sample. This article presents a high-level introduction to techniques often used for chemical analysis during failure analysis. It describes the general considerations for bulk and microscale chemical analysis in failure analysis, the most effective techniques to use for organic or inorganic materials, and examples of using these techniques. The article discusses the processes involved in the chemical analysis of nonmetallics. Advances in chemical analysis methods for failure analysis are also covered.
Series: ASM Handbook
Volume: 11
Publisher: ASM International
Published: 15 January 2021
DOI: 10.31399/asm.hb.v11.a0006762
EISBN: 978-1-62708-295-2
.... “ Research and Citation Resources ,” Purdue University Online Writing Lab , 01 Sept 2019 , https://owl.purdue.edu/owl/research_and_citation/resources.html 4. Katzoff S. , Clarity in Technical Report Writing, National Aeronautics and Space Administration (NASA) , Langley Research Center...
Abstract
As a failure investigation progresses, the time arrives when the data and results of the various testing and analyses are compiled, compared, and interpreted. Data interpretation should be relatively straightforward for results that align well. However, interpretation can be challenging when results from various tests seem contradictory or inconclusive. Regardless, conclusions must eventually be drawn from the data. This article discusses the processes involved in reviewing data, formulating conclusions, failure analysis report preparation and writing, and providing recommendations and follow-up with appropriate personnel to prevent future failures.
Series: ASM Handbook
Volume: 11B
Publisher: ASM International
Published: 15 May 2022
DOI: 10.31399/asm.hb.v11B.a0006915
EISBN: 978-1-62708-395-9
Abstract
This article provides practical information and data on property development in engineering plastics. It discusses the effects of composition on submolecular and higher-order structure and the influence of plasticizers, additives, and blowing agents. It examines stress-strain curves corresponding to soft-and-weak, soft-and-tough, hard-and-brittle, and hard-and-tough plastics and temperature-modulus plots representative of polymers with different degrees of crystallinity, cross-linking, and polarity. It explains how viscosity varies with shear rate in polymer melts and how processes align with various regions of the viscosity curve. It discusses the concept of shear sensitivity, the nature of viscoelastic properties, and the electrical, chemical, and optical properties of different plastics. It also reviews plastic processing operations, including extrusion, injection molding, and thermoforming, and addresses related considerations such as melt viscosity and melt strength, crystallization, orientation, die swell, melt fracture, shrinkage, molded-in stress, and polymer degradation.
Book: Composites
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003476
EISBN: 978-1-62708-195-5
... polymerization of monomer reactants (PMR) polyimides at the National Aeronautics and Space Administration (NASA) Lewis (now NASA Glenn) Research Center (Ref 1 , 2 , and 3 ) and their commercialization by prepreg suppliers, the fiber-reinforced PMR polyimide based on PMR-15 has found increased acceptance...
Abstract
High-temperature-resistant polymers are used in aerospace, electronic, and other applications that demand outstanding elevated-temperature physical and mechanical properties. This article discusses the general characteristics of condensation-type polyimides and polymerization of monomer reactants (PMR) polyimides. It provides information on the applications of PMR-15 with illustrations.
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Published: 01 January 2001
Fig. 5 Thermally stable bench for the far-ultraviolet spectroscopic Explorer spacecraft. Courtesy of NASA/Swales/Alliant Techsystems
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Published: 15 December 2019
Fig. 15 L aser-induced breakdown spectroscopy system ChemCam on the Mars rover Curiosity. Courtesy of NASA/JPL-Caltech
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Published: 01 January 1993
Fig. 2 Diagram showing the increase in the concentration of “space debris” encountered in orbit. Courtesy of D.J. Kessler, NASA Johnson Space Center
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in Refractory Metals and Alloys
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Fig. 36 Location and structure of tungsten fibers in fiber-reinforced superalloy composite turbine blades for rocket engine turbopumps. Courtesy NASA Lewis Research Center
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