Gotowe bibliografie tematyczne / Nuclear rocket engine

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  1. Artykuły w czasopismach
  2. Rozprawy doktorskie
  3. Książki
  4. Części książek
  5. Streszczenia konferencji
  6. Raporty organizacyjne

Gotowa bibliografia na temat „Nuclear rocket engine”

Autor: Grafiati
Data publikacji: 2 czerwca 2025
Data aktualizacji: 31 lipca 2025

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Artykuły w czasopismach na temat "Nuclear rocket engine"

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Лазарева, Ю. И., С. В. Клименко, А. В. Кулик та И. В. Лазарев. "АНАЛИЗ СОВРЕМЕННОГО СОСТОЯНИЯ И ПЕРСПЕКТИВЫ РАЗВИТИЯ РАКЕТНЫХ ДВИГАТЕЛЕЙ ДЛЯ ИССЛЕДОВАНИЯ ДАЛЬНЕГО КОСМОСА". System design and analysis of aerospace technique characteristics 27, № 2 (2022): 50–58. http://dx.doi.org/10.15421/471923.

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The article analyzes the current state and development prospects of rocket engines for space exploration. Currently, for flights to other planets, not to mention the stars, the use of liquid-propellant and solid-propellant rocket engines is becoming increasingly unprofitable, although many rocket engines have been developed. Thus, to reach manned planes even the nearest planets, it is necessary to develop rocket launchers on engines operating on principles different from chemical propulsion systems. The most promising in this regard are electric, laser and nuclear rocket engines, as well as hy
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Zuo, Tianhao. "Designs, Simulations, and Products for Rocket Engines." Highlights in Science, Engineering and Technology 48 (May 16, 2023): 186–91. http://dx.doi.org/10.54097/hset.v48i.8330.

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As a matter of fact, rocket engine technology has developed rapidly in the last 100 years, which plays a crucial role for stellar travelling and detection for astrophysics usages. To be specific, different models, designs and simulation computer software had been developed in order to investigate and explore the dynamic process of the engines as well as evaluate the effectiveness and ability of the rocket engines. With this in mind, this paper gives a basic description of the designs, simulations, and products for rocket engines. In detail, this study will include description of four basic des
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Rawlins, Samantha, and L. Dale Thomas. "Reliability Assessment of Nuclear Thermal Engine Configuration and Health Monitoring System." Journal of the British Interplanetary Society 76, no. 4 (2023): 145–52. http://dx.doi.org/10.59332/jbis-076-04-0145.

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Today’s space nuclear technology programs are often confronted with two fundamental challenges early in the project life cycle: 1) development and testing will be more expensive than a non-nuclear alternative, and 2) the consequences of failure will be more severe. As a result, many space nuclear programs have been designed to minimize testing and maximize their probability of success: their reliability. The United States' Nuclear Engine for Rocket Vehicle Applications Program recognized these facts early on, and by 1961 the program’s primary objective set safety and reliability as the overrid
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Berliand, M., and R. Ishchenko. "CALCULATION OF THE EXPANSION PROCESS OF THE FLOW OF WORKING BODY IN THE NOZZLE OF A LIQUID-PHASE NUCLEAR ROCKET ENGINE." Slovak international scientific journal, no. 95 (May 15, 2025): 86–92. https://doi.org/10.5281/zenodo.15427667.

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In this work, flow parameters of the working body (hydrogen) were calculated at the inlet, throat, and exit sections of the liquid-phase nuclear rocket engine nozzle. A method was proposed for determining the specific impulse of thrust while accounting for losses due to scattering, friction, and variations in the specific enthalpy of the working body caused by non-adiabatic effects. The calculated specific impulse exceeded 9500 m/s, significantly surpassing the performance of chemical rocket engines. The evaluation of the thermogasdynamic parameters of the working body expansion confirmed the
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Kotov, V. M., and S. V. Kotov. "SOLAR ROCKET ENGINES IN NEAR-EARTH SPACE." NNC RK Bulletin 1, no. 4 (2019): 86–90. http://dx.doi.org/10.52676/1729-7885-2019-4-86-90.

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At the current stage of space exploration development, missions to the Moon and geostationary orbit are relevant. Enhancing of power supply level of such missions requires innovative technology development. Nuclear rocket engines and engines with use of solar energy are considered among such technologies. In a number of projects, such engines use intermediate heat energy accumulators, which complicates and increases the cost of construction. This embodiment uses a circuit that enables solar engine to operate with any orientation of the thrust direction towards the sun. The dependence of specif
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Konyukhov, G. V., and A. I. Petrov. "Heat transfer in a nuclear rocket engine." Journal of Engineering Physics and Thermophysics 67, no. 1-2 (1995): 703–6. http://dx.doi.org/10.1007/bf00853318.

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Pilger, Christoph, Patrick Hupe, and Peter Gaebler. "Worldwide detection of rocket launches for space missions using International Monitoring System infrasound arrays." Journal of the Acoustical Society of America 154, no. 4_supplement (2023): A347. http://dx.doi.org/10.1121/10.0023754.

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The signals of rocket launches can be detected at infrasound arrays in thousands of kilometers distance. We use microbarometer arrays, which are part of the International Monitoring System (IMS) for the Comprehensive Nuclear-Test-Ban Treaty (CTBT), to identify and characterize rocket launches all over the world. We studied more than 1000 launch events for space missions and their infrasonic signatures. Even small-lift launch vehicles such as Electron rockets starting from New Zealand with payloads of only a few hundreds of kilograms, e.g., for small satellites, can regularly be detected by one
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Vadim, Zakirov, and Pavshook Vladimir. "Russian nuclear rocket engine design for mars exploration." Tsinghua Science and Technology 12, no. 3 (2007): 256–60. http://dx.doi.org/10.1016/s1007-0214(07)70038-x.

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Brockmeyer, J. W. "Ceramic Matrix Composite Applications in Advanced Liquid Fuel Rocket Engine Turbomachinery." Journal of Engineering for Gas Turbines and Power 115, no. 1 (1993): 58–63. http://dx.doi.org/10.1115/1.2906686.

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Hot gas path components of current generation, liquid fuel rocket engine turbopumps (T/P) are exposed to severe thermal shock, extremely high heat fluxes, corrosive atmospheres, and erosive flows. These conditions, combined with high operating stresses, are severely degrading to conventional materials. Advanced turbomachinery (T/M) applications will impose harsher demands on the turbine materials. These demands include higher turbine inlet temperature for improved performance and efficiency, lower density for improved thrust-to-weight ratio, and longer life for reduced maintenance of re-usable
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Lanin, Anatolii G., and Ivan I. Fedik. "Selecting and using materials for a nuclear rocket engine reactor." Physics-Uspekhi 54, no. 3 (2011): 305–18. http://dx.doi.org/10.3367/ufne.0181.201103f.0319.

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Rozprawy doktorskie na temat "Nuclear rocket engine"

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Gouw, Reza Raymond. "Nuclear design analysis of square-lattice honeycomb space nuclear rocket engine." [Florida] : State University System of Florida, 2000. http://etd.fcla.edu/etd/uf/2000/amt2440/master.pdf.

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Thesis (M.E.)--University of Florida, 2000.<br>Title from first page of PDF file. Document formatted into pages; contains x, 69 p.; also contains graphics. Vita. Includes bibliographical references (p. 68).
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Salamon, Nicholas C. "Analysis of Nuclear Thermal Rocket Engine Coolant Channel Designs Enabled byAdditive Manufacturing." The Ohio State University, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=osu1587590263667569.

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Suzuki, David E. (David Eric). "Development and analysis of startup strategies for a particle bed nuclear rocket engine." Thesis, Massachusetts Institute of Technology, 1993. http://hdl.handle.net/1721.1/49909.

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Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993, and Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Nuclear Engineering, 1993.<br>Includes bibliographical references (leaves ).<br>by David E. Suzuki.<br>M.S.
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Plancher, Johann. "Thermal and fluid design analysis of a square lattice honeycomb nuclear rocket engine." [Gainesville, Fla.] : University of Florida, 2002. http://purl.fcla.edu/fcla/etd/UFE1000154.

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Thesis (M.S.)--University of Florida, 2002.<br>Title from title page of source document. Document formatted into pages; contains xi, 80 p.; also contains graphics. Includes vita. Includes bibliographical references.
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Książki na temat "Nuclear rocket engine"

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Lanin, Anatoly. Nuclear Rocket Engine Reactor. Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-32430-7.

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Lanin, Anatoly. Nuclear Rocket Engine Reactor. Springer Berlin Heidelberg, 2013.

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L, Musgrave Jeffrey, and United States. National Aeronautics and Space Administration., eds. Overview of rocket engine control. National Aeronautics and Space Administration, 1991.

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Robbins, W. H. An historical perspective of the NERVA nuclear rocket engine technology program. Lewis Research Center, 1991.

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United States. National Aeronautics and Space Administration., ed. Robotic planetary science missions enabled with small NTR engine/stage technologies. National Aeronautics and Space Administration, 1995.

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W, Alexander Stephen, and United States. National Aeronautics and Space Administration., eds. "Fast Track" NTR systems assessment for NASA's first lunar outpost scenario. National Aeronautics and Space Administration, 1992.

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United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Nuclear thermal propulsion: A joint NASA/DOE/DOD Workshop : proceedings of the Nuclear Thermal Propulsion Workshop held at the Holiday Inn Strongsville, Ohio. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

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United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, ed. Nuclear thermal propulsion: A joint NASA/DOE/DOD Workshop : proceedings of the Nuclear Thermal Propulsion Workshop held at the Holiday Inn Strongsville, Ohio. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

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United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Nuclear thermal propulsion: A joint NASA/DOE/DOD Workshop : proceedings of the Nuclear Thermal Propulsion Workshop held at the Holiday Inn Strongsville, Ohio. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

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United States. National Aeronautics and Space Administration., ed. The rationale/benefits of nuclear thermal rocket propulsion for NASA'S lunar space transportation system. National Aeronautics and Space Administration, 1991.

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Części książek na temat "Nuclear rocket engine"

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Lanin, Anatoly. "Outlook for Nuclear Rocket Engine Reactors." In Nuclear Rocket Engine Reactor. Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-32430-7_8.

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Lanin, Anatoly. "History Creation of a Nuclear Rocket Engine Reactor." In Nuclear Rocket Engine Reactor. Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-32430-7_1.

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Lanin, Anatoly. "Design of a NRER." In Nuclear Rocket Engine Reactor. Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-32430-7_2.

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Lanin, Anatoly. "Methods of Modeling Tests." In Nuclear Rocket Engine Reactor. Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-32430-7_3.

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Lanin, Anatoly. "Materials of the Reactor Core." In Nuclear Rocket Engine Reactor. Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-32430-7_4.

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Lanin, Anatoly. "Radiation Resistance of the HRA Elements." In Nuclear Rocket Engine Reactor. Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-32430-7_5.

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Lanin, Anatoly. "Corrosion of Materials in the Working Medium." In Nuclear Rocket Engine Reactor. Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-32430-7_6.

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Lanin, Anatoly. "Bearing Capacity of Elements’ HGA." In Nuclear Rocket Engine Reactor. Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-32430-7_7.

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Emrich, William. "Rocket Engine Fundamentals." In Principles of Nuclear Rocket Propulsion. Elsevier, 2016. http://dx.doi.org/10.1016/b978-0-12-804474-2.00002-3.

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Emrich, William. "Rocket engine fundamentals." In Principles of Nuclear Rocket Propulsion. Elsevier, 2023. http://dx.doi.org/10.1016/b978-0-323-90030-0.00011-4.

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Streszczenia konferencji na temat "Nuclear rocket engine"

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Schroll, Mitchell. "Characterization of Engine Cooldown for a Centrifugal Nuclear Thermal Rocket." In IAF Space Propulsion Symposium, Held at the 75th International Astronautical Congress (IAC 2024). International Astronautical Federation (IAF), 2024. https://doi.org/10.52202/078371-0163.

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Blackman, Timothy, Julia Kondrat'yev, Olivia Williams, Robert Frederick, and L. Thomas. "Initial Atmospheric Results for Simulating a Centrifugal Nuclear Thermal Rocket Engine." In Nuclear and Emerging Technologies for Space (NETS 2025). American Nuclear Society, 2025. https://doi.org/10.13182/xyz-47359.

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Agarwal, D. C., Michael Eckhardt, and Theo Hoffmann. "Repair of Alloy Components after Long Term High Temperature Exposure." In CORROSION 2003. NACE International, 2003. https://doi.org/10.5006/c2003-03475.

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Abstract Nickel base alloys are used in a variety of industries where severe corrosive conditions, whether it be aqueous corrosion or high temperature corrosion, are encountered. These alloys for high temperature service, known as superalloys, are utilized at a higher proportion of their actual melting point, approaching or even slightly exceeding 0.9Tm, where Tm is the melting point, than any other class of commercial metallurgical materials. In addition to aircraft, marine and industrial gas turbines, these high temperature alloys see service in space vehicles, rocket engines, submarines, nu
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CULVER, DONALD, and RICHARD ROCHOW. "Unique nuclear thermal rocket engine." In 29th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-1812.

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Culver, Donald W., and Richard Rochow. "Unique nuclear thermal rocket engine." In Proceedings of the tenth symposium on space nuclear power and propulsion. AIP, 1993. http://dx.doi.org/10.1063/1.43214.

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GUNN, STANLEY. "Development of nuclear rocket engine technology." In 25th Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-2386.

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Gunn, Stanley, and Rolv Hundal. "Design of superheat nuclear thermal rocket engine." In 30th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1994. http://dx.doi.org/10.2514/6.1994-2895.

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GUNN, STANLEY, MARGARITA SAVOIE, and ROLV HUNDAL. "Nuclear thermal rocket engine operation and control." In 29th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-2372.

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Lorenzo, Carl F., and Jeffrey L. Musgrave. "Overview of rocket engine control." In Proceedings of the ninth symposium on space nuclear power systems. AIP, 1992. http://dx.doi.org/10.1063/1.41807.

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"Small nuclear thermal rocket engine issues and implications." In Space Programs and Technologies Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-4781.

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Raporty organizacyjne na temat "Nuclear rocket engine"

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Kirk, W. L., J. C. Hedstrom, S. W. Moore, et al. An investigation of dual-mode operation of a nuclear-thermal rocket engine. Office of Scientific and Technical Information (OSTI), 1991. http://dx.doi.org/10.2172/5650128.

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Koehlinger, M. W., R. G. Bennett, C. G. Motloch, and M. M. Gurfink. Gas core nuclear thermal rocket engine research and development in the former USSR. Office of Scientific and Technical Information (OSTI), 1992. http://dx.doi.org/10.2172/10147766.

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Koehlinger, M. W., R. G. Bennett, and M. M. Gurfink. Gas core nuclear thermal rocket engine research and development in the former USSR. Edited by C. G. Motloch. Office of Scientific and Technical Information (OSTI), 1992. http://dx.doi.org/10.2172/6630912.

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Friesen, H. N. Radiological effluents released from nuclear rocket and ramjet engine tests at the Nevada Test Site 1959 through 1969: Fact Book. Office of Scientific and Technical Information (OSTI), 1995. http://dx.doi.org/10.2172/101088.

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Noone, Emily, and Lydia Harriss. Hypersonic missiles. Parliamentary Office of Science and Technology, 2023. http://dx.doi.org/10.58248/pn696.

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This POSTnote looks at hypersonic missile technologies, efforts to develop them, potential applications, and the possible challenges they may present for missile defence and global stability. Key Points: • Hypersonic missiles combine speeds of over five times the speed of sound with significant manoeuvrability during flight. • Their manoeuvrability enables them to change trajectory during flight, making their flight-path and target difficult to predict. • They fly at lower altitudes than ballistic missiles, which means that they may be harder to track at long distances with some surface-based
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