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Books on the topic 'Ion engines'

Author: Grafiati
Published: 4 June 2021
Last updated: 12 February 2022

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1

Starling, Dan A. Propellant feed control for ion engines. Monterey, Calif: Naval Postgraduate School, 1996.

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2

Foster, John E. Inter-cusp ion and electron transport in a NSTAR-derivative ion thruster. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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3

Foster, John E. Inter-cusp ion and electron transport in a NSTAR-derivative ion thruster. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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4

Foster, John E. Inter-cusp ion and electron transport in a NSTAR-derivative ion thruster. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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5

Foster, John E. Inter-cusp ion and electron transport in a NSTAR-derivative ion thruster. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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6

Foster, John E. Internal plasma properties and enhanced performance of an 8-cm ion thruster discharge. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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7

Rawlin, Vincent K. Thermal environmental testing of NSTAR engineering model ion thrusters. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1999.

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8

International Electric Propulsion Conference (24th 1995 Moscow, Russia). Proceedings of the 24th International Electric Propulsion Conference: IEPC. [S.l: s.n., 1995.

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9

Stuart, Thomas A. Study of a high voltage ion engine power supply: NASA grant NAG3-1576. [Washington, DC: National Aeronautics and Space Administration, 1996.

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10

Foster, John E. Enhanced discharge performance in a ring cusp plasma source. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2000.

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11

Val'eho, Mal'donado, and Nikolay Chaynov. Calculation of kinematics and dynamics of inline piston engines. ru: INFRA-M Academic Publishing LLC., 2021. http://dx.doi.org/10.12737/1058850.

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The textbook discusses the kinematics and dynamics of inline piston internal combustion engines with axial and deaxial crank mechanism. The necessary material for calculating the forces and moments acting in the engine is given, the balancing of engines, the construction of vector diagrams of pressure on the crankshaft bearings are considered, examples of calculations are given. Meets the requirements of the federal state educational standards of higher education of the latest generation. For students of higher educational institutions studying in the field of training "Energy engineering".
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12

Bruce, Lisa. Engines, engines. London: Bloomsbury Children's, 2001.

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13

W, Awdry. Tramway engines. London: Heinemann, 1995.

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14

The engines of our ingenuity: An engineer looks at technology and culture. Oxford: Oxford University Press, 2000.

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15

ill, Iwai Melissa, ed. Good night engines. New York: Clarion Books, 2003.

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16

Mortensen, Denise Dowling. Good night, engines. New York: Clarion Books, 2003.

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17

Calmenson, Stephanie. Engine, engine, number nine. New York: Hyperion Books for Children, 1996.

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18

Calmenson, Stephanie. Engine, engine, number nine. New York: Scholastic, 1996.

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19

Engineers, Society of Automotive, ed. Deposits in modern engines. Warrendale, PA: Society of Automotive Engineers, 1988.

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20

Vallejo Maldonado, Pablo Ramon, and Nikolay Chaynov. Kinematics and dynamics of automobile piston engines. ru: INFRA-M Academic Publishing LLC., 2019. http://dx.doi.org/10.12737/989072.

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The fundamentals of kinematics and dynamics of transport piston internal combustion engines made using different layout schemes are presented. Along with the traditional in-line, V-shaped, including oppositional, arrangement of cylinders, schemes with "staggered" arrangement of cylinders in the block at the displaced connecting rod necks of the crankshaft of the engine are considered. The kinematics of the coaxial crank mechanism is considered in detail. The questions of dynamics with reduction of calculated dependences of forces, moments, a choice of a rational order of work of cylinders in relation to the considered kinematic schemes are in detail stated. Considerable attention is paid to the unevenness of the crankshaft rotation speed and engine balancing. The loads on the main and connecting rod bearings of the crankshaft, the knowledge of which is necessary in determining the bearing capacity of bearing units, are also considered. Meets the requirements of the Federal state educational standards of higher education of the last generation. For students of higher educational institutions studying in the direction of training 23.03.03 "Operation of transport and technological machines and complexes" and related areas.
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21

Steve Jobs: Apple icon. Minneapolic, MN: ABDO Pub. Co., 2012.

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22

W, Awdry. Gallant old engine. London: Heinemann, 1987.

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23

W, Awdry. Gallant old engine. London: Heinemann, 1995.

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24

Allcroft, Britt. Little engines can do big things. New York: Random House, 2000.

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25

Propellant Feed Control for Ion Engines. Storming Media, 1996.

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26

Low-power ion thruster development status. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1999.

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27

Low-power ion thruster development status. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1999.

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28

Low-power ion thruster development status. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1999.

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29

Center, Lewis Research, ed. Low-power ion thruster development status. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1999.

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30

Ion Based Pressure Sensor for Pulse Detonation Engines. Storming Media, 2004.

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31

Closed-drift thruster investigations. Fort Collins, Colo: Dept. of Physics, Colorado State University, 1986.

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32

D, Schemmel Terry, Patterson Michael J. 1955-, and Lewis Research Center, eds. Closed-drift thruster investigations. Fort Collins, Colo: Dept. of Physics, Colorado State University, 1986.

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33

N, Matossian J., and United States. National Aeronautics and Space Administration., eds. Mercury ion thruster technology. [Washington, DC: National Aeronautics and Space Administration, 1989.

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34

Center, NASA Glenn Research, ed. Design and performance of 40 cm ion optics. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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35

Center, NASA Glenn Research, ed. Design and performance of 40 cm ion optics. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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36

Scaling of ion thrusters to low power. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

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37

Center, NASA Glenn Research, ed. Improving the total impulse capability of the NSTAR ion thruster with thick-accelerator-grid ion optics. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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38

Center, NASA Glenn Research, ed. Improving the total impulse capability of the NSTAR ion thruster with thick-accelerator-grid ion optics. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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39

Hall thruster ion beam characterization. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

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40

K, Rawlin Vincent, and United States. National Aeronautics and Space Administration., eds. Recycle requirements for NASA's 30cm xenon ion thruster. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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41

K, Rawlin Vincent, and United States. National Aeronautics and Space Administration., eds. Recycle requirements for NASA's 30cm xenon ion thruster. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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42

United States. National Aeronautics and Space Administration., ed. Impingement-current-erosion characteristics of accelerator grids on two-grid ion thrusters: Under grant NAG3-1801. [Washington, DC: National Aeronautics and Space Administration, 1996.

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43

Impingement-current-erosion characteristics of accelerator grids on two-grid ion thrusters: Under grant NAG3-1801. [Washington, DC: National Aeronautics and Space Administration, 1996.

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44

United States. National Aeronautics and Space Administration., ed. Impingement-current-erosion characteristics of accelerator grids on two-grid ion thrusters: Under grant NAG3-1801. [Washington, DC: National Aeronautics and Space Administration, 1996.

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45

United States. National Aeronautics and Space Administration., ed. Impingement-current-erosion characteristics of accelerator grids on two-grid ion thrusters: Under grant NAG3-1801. [Washington, DC: National Aeronautics and Space Administration, 1996.

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46

United States. National Aeronautics and Space Administration., ed. Stationary plasma thruster ion velocity distributions. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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47

High-power ion thruster technology. [Washington, DC]: National Aeronautics and Space Administration, 1996.

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48

N, Matossian J., and United States. National Aeronautics and Space Administration., eds. High-power ion thruster technology. [Washington, DC]: National Aeronautics and Space Administration, 1996.

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49

N, Matossian J., and United States. National Aeronautics and Space Administration., eds. High power ion thruster technology. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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50

N, Matossian J., and United States. National Aeronautics and Space Administration., eds. High-power ion thruster technology. [Washington, DC]: National Aeronautics and Space Administration, 1996.

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