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Books on the topic 'Adaptive thermal protection systems'

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Author: Grafiati
Published: 30 May 2022
Last updated: 31 May 2022

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1

Institute, American National Standards. Standard for thermal protectors for motors. 7th ed. Northbrook, Ill: Underwriters' Laboratories, 1991.

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2

Scotti, Stephen J. Current Technology for Thermal Protection Systems: Proceedings of a workshop sponsored by the National Aeronautics and Space Administration, Washington, D.C., and held at Langley Research Center, Hampton, Virginia, February 11-12, 1992. Hampton, Va: Langley Research Center, 1992.

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3

Knoll, Richard H. Design, development, and test of shuttle/Centaur G-prime cryogenic tankage thermal protection systems. [Washington, DC: National Aeronautics and Space Administration, 1987.

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4

E, Myers David. Parametric weight comparison of advanced metallic, ceramic tile and ceramic blanket thermal protection systems. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2000.

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5

Steinberg, Dave S. Preventing thermal cycling and vibration failures in electronic equipment. New York: J. Wiley, 2001.

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6

Mihaylov, Vyacheslav, Elena Sotnikova, and Nina Kalpina. Eco-friendly air protection systems for motor transport facilities. ru: INFRA-M Academic Publishing LLC., 2022. http://dx.doi.org/10.12737/1093106.

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The textbook considers the issue of assessing the heat and humidity state of air in the processes of its processing in various systems, provides requirements for air protection means, taking into account their environmental friendliness, shows ways of energy saving in cooling, heating and year-round air conditioning systems, as well as when protecting the atmosphere from harmful emissions. The way of energy saving with individual thermal protection of the operator by means of local cooling during air treatment in an irrigated intensified nozzle is shown and recommendations for reducing its material consumption are developed. The method and means of reducing the toxicity of emissions of tractor internal combustion engines during its operation in rooms of limited volume by water vapor humidification of the fuel-air mixture are demonstrated. The ways of noise reduction of air protection systems are shown. Meets the requirements of the federal state educational standards of higher education of the latest generation. It is intended for students studying in the specialties "Ground transport and technical means", "Operation of transport and technological machines and complexes", "Power engineering", "Ground transport and technological complexes", "Refrigeration, cryogenic equipment and life support systems", "Technosphere safety", "Ecology and nature management".
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7

European Workshop on Hot Structures and Thermal Protection Systems for Space Vehicle (4th 2002 Palermo, Italy). The 4th European Workshop on Hot structures and thermal protection systems for space vehicle: 26-29 November 2002, Palermo, Italy. Noordwijk: ESA Publications Division, 2003.

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8

Wilkinson, John P. Space shuttle production verification motor 1 (PV-1) field joint protection system.: Final report. Brigham City, UT: Thiokol Corp., Space Operations, 1990.

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9

Gibbins, Martin N. Systems integration and demonstration of advanced reusable structure for ALS. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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10

Kuhn, Gary D. Postflight aerothermodynamic analysis of Pegasus[copyright] using computational fluid dynamic techniques. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1992.

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11

Kramarov, Sergey, Vladimir Khramov, Elena Grebenyuk, and Anatoly Bocharov. Fundamentals of the ergotechnical approach to the formation of an electronic educational environment. ru: Publishing Center RIOR, 2021. http://dx.doi.org/10.29039/02086-9.

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The monograph deals with the problems of analysis and synthesis of electronic information and learning environment as an ergatic system. The issues of creation, development and evaluation of such systems, as well as information support of the process of building and using artificial intelligence, including in the protection of information, are considered. The monograph provides theoretical justifications for the research of information objects, which reveals the mechanism of constructing a mathematical model of the educational process at the university and explains the understanding of the education system as a system of systems, as well as information processes associated with it. The research presented in the monograph is the basis for the creation of new and effective robotic organizational and organizational-technical systems in education. The monograph is intended for researchers and teachers, postgraduates, undergraduates and engineers specializing in the field of educational management, including intelligent adaptive control of complex robotic systems.
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12

Duffa, Georges. Ablative Thermal Protection Systems Modeling. Amer Inst of Aeronautics &, 2013.

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13

A, Kourtides Demetrius, and Ames Research Center, eds. Evaluation of thermal control coatings for flexible ceramic thermal protection systems. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1997.

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14

Schnitzer, Pascale. How to Target Households in Adaptive Social Protection Systems? World Bank, Washington, DC, 2016. http://dx.doi.org/10.1596/25387.

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15

M, Sawko Paul, and Ames Research Center, eds. Thermal degradation study of silicon carbide threads developed for advanced flexible thermal protection systems. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.

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16

K, Davis Christopher, and United States. National Aeronautics and Space Administration., eds. Shearographic non-destructive evaluation of space shuttle thermal protection systems. [Washington, DC: National Aeronautics and Space Administration, 1995.

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17

J, Scotti Stephen, United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., and Langley Research Center, eds. Current technology for thermal protection systems: Proceedings of a workshop. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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18

K, Davis Christopher, and United States. National Aeronautics and Space Administration., eds. Shearographic non-destructive evaluation of space shuttle thermal protection systems. [Washington, DC: National Aeronautics and Space Administration, 1995.

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19

K, Davis Christopher, and United States. National Aeronautics and Space Administration., eds. Shearographic non-destructive evaluation of space shuttle thermal protection systems. [Washington, DC: National Aeronautics and Space Administration, 1995.

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20

Joseph, Scotti Stephen, United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., and Langley Research Center, eds. Current technology for thermal protection systems: Proceedings of a workshop. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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21

K, Davis Christopher, and United States. National Aeronautics and Space Administration., eds. Shearographic non-destructive evaluation of space shuttle thermal protection systems. [Washington, DC: National Aeronautics and Space Administration, 1995.

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22

Center, Langley Research, ed. Development of metallic thermal protection systems for the reusable launch vehicle. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

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23

K, Tran Huy, and Ames Research Center, eds. Phenolic Impregnated Carbon Ablators (PICA) as thermal protection systems for discovery missions. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1997.

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24

Second European Workshop on thermal protection systems: Held Stuttgart 23-25 October 1995. Paris: European Space Agency, 1996.

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25

United States. National Aeronautics and Space Administration., ed. Flight set 360L007 (STS-33R): Field joint protection system, thermal protection system, and systems tunnel components : final report. Brigham City, UT: Thiokol Corp., Space Operations, 1990.

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26

United States. National Aeronautics and Space Administration., ed. Flight set 360L007 (STS-33R): Field joint protection system, thermal protection system, and systems tunnel components : final report. Brigham City, UT: Thiokol Corp., Space Operations, 1990.

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27

Steinberg, Dave S. Preventing Thermal Cycling and Vibration Failures in Electronic Equipment. Wiley-Interscience, 2001.

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28

United States. National Aeronautics and Space Administration., ed. Advances in hypersonic vehicle synthesis with application to studies of advanced thermal protection systems: Final report. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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29

United States. National Aeronautics and Space Administration., ed. Advances in hypersonic vehicle synthesis with application to studies of advanced thermal protection systems: Final report. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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30

Schnitzer, Pascale. How to Target Households in Adaptive Social Protection Systems? Evidence from Humanitarian and Development Approaches in Niger. Taylor and Francis, 2019. http://dx.doi.org/10.1596/33145.

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31

Kessler, Günter. Sustainable and Safe Nuclear Fission Energy: Technology and Safety of Fast and Thermal Nuclear Reactors (Power Systems). Springer, 2012.

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32

Italiana, Agenzia Spaziale. The 4th European Workshop on Hot Structures and Thermal Protection Systems for Space Vehicle: 26-29 November 2002, Palermo, Italy. ESA Publications, 2003.

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33

thermiciens, Société française des, and International Institute of Refrigeration, eds. Thermal protection of man under hot and hazardous conditions: Operational requirements, physiological and technological parameters, protection against steam, microcooling systems for thermal assistance, improvement of ergonomics characteristics, testing methods and protocols, simulation : 24, 25 & 26 March 1999, Paris, France. [Paris: Société?], 1999.

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34

Engineering aerothermal analysis for X-34 thermal protection system design: 36th Aerospace Sciences meeting & exhibit : January 12-15, 1998/Reno, NV. Reston, VA: American Institute of Aeronautics and Astronautics, 1998.

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35

Operations, Thiokol Corporation Space, and George C. Marshall Space Flight Center., eds. Flight set 360L001 (STS-26) igniter, post flight, final report. Brigham City, UT: Thiokol Corp., Space Operations, 1990.

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36

Operations, Thiokol Corporation Space, and George C. Marshall Space Flight Center., eds. Flight set 360L001 (STS-26) igniter, post flight, final report. Brigham City, UT: Thiokol Corp., Space Operations, 1990.

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37

Operations, Thiokol Corporation Space, and George C. Marshall Space Flight Center., eds. Flight set 360L001 (STS-26) igniter, post flight, final report. Brigham City, UT: Thiokol Corp., Space Operations, 1990.

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38

Nicolici, Nicola. Power-Constrained Testing of Vlsi Circuits: A Guide To The Ieee 1149.4 Test Standard. Springer, 2010.

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39

Power-Constrained Testing of VLSI Circuits (Frontiers in Electronic Testing). Springer, 2003.

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40

Einhorn Yaffee Prescott Architecture and Engineering, P.C., McMullan & Associates., and A. Morton Thomas and Associates., eds. Lincoln Memorial structural monitoring report for skylight room, Washington, D.C.: Final submission. Albany, NY: Einhorn Yaffee Prescott Architecture & Engineering, 1992.

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41

A, Breckenridge Roger, and Langley Research Center, eds. Technology for the future: In-Space Technology Experiments Program. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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42

A, Breckenridge Roger, and Langley Research Center, eds. Technology for the future: In-Space Technology Experiments Program. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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43

Galley, Helen F., and Heather M. Wilson. Immune system physiology in anaesthetic practice. Edited by Jonathan G. Hardman. Oxford University Press, 2017. http://dx.doi.org/10.1093/med/9780199642045.003.0010.

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The immune system provides protection against invading pathogens, foreign cells including tumour cells, and macromolecules. It comprises an early, non-specific, innate immune response and a later, specific, adaptive immune response that helps prevent disease or recurrence of disease. Innate and adaptive immune systems work together with mutual interactivity distinguishing ‘self’ from ‘non-self components’ to provide effective immune responses and prevent infection. This chapter describes the basic processes involved in immune responses and illustrates the particular relevance for some disease processes as well as highlighting stresses associated with anaesthesia and surgery that can modulate responses.
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