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1

Ballard, Michael A. Impacts of electric propulsion systems on submarine design. Available from the National Technical Information Service, 1989.

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2

Woud, Hans Klein. Design of propulsion and electric power generation systems. IMarEST, Institute of Marine Engineering, Science and Technology, 2002.

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3

Woud, Hans Klein. Design of propulsion and electric power generation systems. IMarEST, Institute of Marine Engineering, Science and Technology, 2002.

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4

Douwe, Stapersma, ed. Design of propulsion and electric power generation systems. IMarEST, Institute of Marine Engineering, Science and Technology, 2002.

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5

Weldon, Vincent. Design optimization of gas generator hybrid propulsion boosters. National Aeronautics and Space Administration, 1990.

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6

Kucinski, William. So You Want to Design Engines: UAV Propulsion Systems. SAE International, 2018. http://dx.doi.org/10.4271/sywd-0003.

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7

Kumar, S. Kishore, Indira Narayanaswamy, and V. Ramesh, eds. Design and Development of Aerospace Vehicles and Propulsion Systems. Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-9601-8.

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8

Klineberg, John M. Advances in computational design and analysis of airbreathing propulsion systems. National Aeronautics and Space Administration, 1989.

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9

Chamis, C. C. Multi-disciplinary coupling effects for integrated design of propulsion systems. National Aeronautics and Space Administration, 1993.

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10

Chamis, C. C. Multi-disciplinary coupling effects for integrated design of propulsion systems. National Aeronautics and Space Administration, 1993.

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11

Chamis, C. C. Multi-disciplinary coupling effects for integrated design of propulsion systems. National Aeronautics and Space Administration, 1993.

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12

Hartley, T. T. Improved large perturbation propulsion models for control system design (1988-89) & Large perturbation models of high velocity propulsion systems (1989-1990) & Reduced order propulsion models for control system design (1990-1991). University of Akron, 1991.

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13

Garg, Sanjay. Integrated flight/propulsion control system design based on a centralized approach. National Aeronautics and Space Administration, 1989.

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14

Guzzella, Lino. Vehicle Propulsion Systems: Introduction to Modeling and Optimization. 3rd ed. Springer Berlin Heidelberg, 2013.

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15

Long, K. F. Deep space propulsion: A roadmap to interstellar flight. Springer, 2012.

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16

Kingsbury, Nancy R. Space nuclear propulsion: History, cost, and status of programs : statement of Nancy R. Kingsbury, Director, Air Force Issues, National Security and International Affairs Division, before the Subcommittee on Investigations and Oversight, Committee on Science, Space, and Technology, House of Representatives. The Office, 1992.

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17

Franklin, James A. Criteria for design of integrated flight/propulsion control systems for STOVL fighter aircraft. National Aeronautics and Space Administration, Ames Research Center, 1993.

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18

Franklin, James A. Criteria for design of integrated flight/propulsion control systems for STOVL fighter aircraft. National Aeronautics and Space Administration, Ames Research Center, 1993.

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19

Garg, Sanjay. Integrated flight/propulsion control design for a STOVL aircraft using H-infinity control design techniques. Lewis Research Center, 1991.

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20

T, Zhdanov V., Kurziner R. I, Komissii͡a po razrabotke nauchnogo nasledii͡a F.A. T͡Sandera. та Kharkivsʹkyĭ aviat͡siĭnyĭ instytut imeni M.I͡E. Zhukovskoho., ред. Trudy Vosʹmykh chteniĭ, posvi͡ashchennykh razrabotke nauchnogo nasledii͡a i razvitii͡u ideĭ F.A. T͡Sandera: Sekt͡sii͡a "Teorii͡a i konstrukt͡sii͡a dvigateleĭ letatelʹnykh apparatov". IIET AN SSSR, 1989.

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21

Pavlovich, Mishin Vasiliĭ, Komissii͡a po razrabotke nauchnogo nasledii͡a F.A. T͡Sandera. та Kharkivsʹkyĭ aviat͡siĭnyĭ instytut imeni M.I͡E. Zhukovsʹkoho., ред. Trudy Vosʹmykh chteniĭ, posvi͡ashchennykh razrabotke nauchnogo nasledii͡a i razvitii͡u ideĭ F.A. T͡Sandera: Sekt͡sii͡a "Teorii͡a i konstrukt͡sii͡a letatelʹnykh apparatov". IIEiT AN SSSR, 1985.

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22

Chtenii͡a, posvi͡ashchennye razrabotke nauchnogo nasledii͡a i razvitii͡u ideĭ F.A. T͡Sandera (8th 1983 Kharkiv, Ukraine). Trudy Vosʹmykh chteniĭ, posvi͡ashchennykh razrabotke nauchnogo nasledii͡a i razvitii͡u ideĭ F.A. T͡Sandera: Sekt͡sii͡a "Ėnergosilovye ustanovki kosmicheskikh apparatov". IIET AN SSSR, 1986.

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23

California Institute of Technology, Pasadena. Jet Propulsion Laboratory. Observational Systems Division: Conceive, design, develop, test, and implement scientific instruments for remotely viewing and measuring the Earth, the solar system, the galaxy, and the universe. National Aeronautics and Space Administration, Jet Propulsion Laboratory, California Institute of Technology, 1989.

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24

California, Institute of Technology Pasadena Jet Propulsion Laboratory. Observational Systems Division: Conceive, design, develop, test, and implement scientific instruments for remotely viewing and measuring the Earth, the solar system, the galaxy, and the universe. National Aeronautics and Space Administration, Jet Propulsion Laboratory, California Institute of Technology, 1989.

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25

Robinson, Philip J. Space station auxiliary thrust chamber technology: Final report 2210-90-FFR. Lewis Research Center, National Aeronautics and Space Administration, 1990.

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26

Garg, Sanjay. Application of an integrated methodology for propulsion and airframe control design to a STOVL aircraft. National Aeronautics and Space Administration, 1994.

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27

Space shuttle main engine: The first twenty years and beyond. AAS Publications Office, 2008.

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28

Schmidt, D. K. Cooperative control theory and integrated flight and propulsion control: Final technical report for grant NAG3-575 covering the period 1994-1995. Dept. of Aerospace Engineering, University of Maryland, 1995.

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29

George, Russell J. Flight motor set 360L001 (STS-26R): Final report. Thiokol Corp., Space Operations, 1989.

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30

George, Russell J. Flight motor set 360L001 (STS-26R): Final report. Thiokol Corp., Space Operations, 1989.

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31

Chernicoff, William P. Clean air program: Design guidelines for bus transit systems using electric and hybrid electric propulsion as an alternative fuel. Federal Transit Administration, Office of Research, Demonstration, and Innovation, 2003.

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32

Roskam, Jan. Design, analysis and control of large transports so that control of engine thrust can be used as a back-up of the primary flight controls: Final technical report, grant #NAG 2-789. University of Kansas, Center for Research, Inc., 1995.

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33

C, Oates Gordon, ed. Aircraft propulsion systems technology and design. American Institute of Aeronautics and Astronautics, 1989.

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34

Sun, Zongxuan, and Guoming G. Zhu. Design and Control of Automotive Propulsion Systems. Taylor & Francis Group, 2014.

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35

Design and Control of Automotive Propulsion Systems. Taylor & Francis Group, 2014.

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36

Sun, Zongxuan, and Guoming G. Zhu. Design and Control of Automotive Propulsion Systems. CRC Press, 2014. http://dx.doi.org/10.1201/b17947.

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37

Multimegawatt electric propulsion system design considerations. National Aeronautics and Space Administration, 1991.

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38

E, Parkes James, Mantenieks Maris A, and United States. National Aeronautics and Space Administration., eds. Multimegawatt MPD thruster design considerations. National Aeronautics and Space Administration, 1992.

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39

R, Whitley M., Knight K. C, and George C. Marshall Space Flight Center., eds. Comprehensive design reliability activities for aerospace propulsion systems. National Aeronautics and Space Administration, Marshall Space Flight Center, 2000.

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40

C, Rapp Douglas, and United States. National Aeronautics and Space Administration., eds. Design issues for propulsion systems using metallized propellants. National Aeronautics and Space Administration, 1991.

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41

R, Whitley M., Knight K. C, and George C. Marshall Space Flight Center., eds. Comprehensive design reliability activities for aerospace propulsion systems. National Aeronautics and Space Administration, Marshall Space Flight Center, 2000.

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42

United States. National Aeronautics and Space Administration., ed. Mechanical flexible joint design document. Sverdrup Corp., 1993.

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43

Mechanical flexible joint design document. Sverdrup Corp., 1993.

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44

W, Lee C., Strickland Matthew 1962-, and Langley Research Center, eds. Design of an integrated airframe/propulsion control system architecture. National Aeronautics and Space Administration, Langley Research Center, 1990.

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45

Design of a thrust stand for high power electric propulsion devices. National Aeronautics and Space Administration, 1990.

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46

N, Singhal Surendra, and United States. National Aeronautics and Space Administration., eds. Multi-disciplinary coupling effects for integrated design of propulsion systems. National Aeronautics and Space Administration, 1993.

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47

Haddad, Wassim M., VijaySekhar Chellaboina, and Alexander Leonessa. Hierarchical Nonlinear Switching Control Design with Applications to Propulsion Systems. Springer, 2000.

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48

Hierarchical nonlinear switching control design with applications to propulsion systems. Springer London, 2000. http://dx.doi.org/10.1007/bfb0110129.

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49

Orbital transfer vehicle engine technology: Baffled injector design, fabrication and verification. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

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50

Design verification test matrix development for the STME thrust chamber assembly. National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1993.

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