Gotowe bibliografie tematyczne / Cryogenic oxygen storage

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Gotowa bibliografia na temat „Cryogenic oxygen storage”

Autor: Grafiati

Data publikacji: 3 czerwca 2025

Data aktualizacji: 31 lipca 2025

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Artykuły w czasopismach na temat "Cryogenic oxygen storage"

Melag, Leena, M. Munir Sadiq, Kristina Konstas, Farnaz Zadehahmadi, Kiyonori Suzuki, and Matthew R. Hill. "Performance evaluation of CuBTC composites for room temperature oxygen storage." RSC Advances 10, no. 67 (2020): 40960–68. http://dx.doi.org/10.1039/d0ra07068h.

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Hanak, Dawid, and Vasilije Manovic. "Techno-economic analysis of oxy-combustion coal-fired power plant with cryogenic oxygen storage." Applied Energy 191 (January 16, 2017): 193–203. https://doi.org/10.1016/j.apenergy.2017.01.049.

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Around 43% of the cumulative CO<sub>2</sub> emission from the power sector between 2012 and 2050 could be mitigated through implementation of carbon capture and storage, and utilisation of renewable energy sources. Energy storage technologies can increase the efficiency of energy utilisation and thus should be widely deployed along with low-emission technologies. This study evaluates the techno-economic performance of cryogenic O<sub>2</sub> storage implemented in an oxy-combustion coal-fired power plant as a means of energy storage. Such system was found to have high energy density and specif

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Portillo, E., Luz M. Gallego Fernández, M. Cano, B. Alonso-Fariñas, and B. Navarrete. "Techno-Economic Comparison of Integration Options for an Oxygen Transport Membrane Unit into a Coal Oxy-Fired Circulating Fluidized Bed Power Plant." Membranes 12, no. 12 (2022): 1224. http://dx.doi.org/10.3390/membranes12121224.

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The inclusion of membrane-based oxygen-fired combustion in power plants is considered an emerging technology that could reduce carbon emissions in a more efficient way than cryogenic oxygen-fired processes. In this paper, a techno-economic assessment was developed for a 863 MWel,net power plant to demonstrate whether this CCS technique results in a reduction in efficiency losses and economic demand. Four configurations based on oxygen transport membranes were considered, while the benchmark cases were the air combustion process without CO2 capture and a cryogenic oxygen-fired process. The type

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Swanger, A. M., R. Fernando, C. Mahony, R. Carro, and A. Harrison. "Cryogenic Modules for Synergistic O₂ Generation and CO₂ Retention in Closed-Circuit Escape Respirators." IOP Conference Series: Materials Science and Engineering 1301, no. 1 (2024): 012044. http://dx.doi.org/10.1088/1757-899x/1301/1/012044.

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Abstract Since 2018, NASA and the National Institute for Occupational Safety and Health (NIOSH) have been developing a liquid oxygen storage module (LOXSM) based on the NASA patent-pending Cryogenic Flux Capacitor (CFC) technology. LOXSM’s could potentially replace the gaseous or chemical-based oxygen supply in current closed-circuit escape respirators (CCER), with reducing CCER size being a primary goal. By virtue of the CFC functionality, cryogenic oxygen stored within the LOXSM is released in response to heat input, ideally from the breathing loop. Prior efforts focused on the oxygen storag

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Braverman, V. Ya, H. V. Zhuk, and B. K. Ilienko. "TECHNOLOGIES OF CRYOGENIC STORAGE OF ELECTRICITY FROM RENEWABLE SOURCES." Energy Technologies & Resource Saving, no. 4 (December 20, 2022): 45–50. http://dx.doi.org/10.33070/etars.4.2022.04.

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The peculiarities of storing electricity produced by traditional systems of its production and using renewable energy sources are considered, the state of the problem is discussed. Examples of industrial application of electricity storage systems using compressed and liquefied air are given. Liquid air storage systems have been shown to be the most efficient. A scheme for the accumulation of electricity and its production with the use of turbo-expander power generator units with the use of liquefied air is proposed. Taking into account the situation that has developed in Ukraine in connection

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Voronetskiy, A. V. "Comparative analysis of operational indicators of air separation plants." Glavnyj mekhanik (Chief Mechanic), no. 3 (February 25, 2022): 188–202. http://dx.doi.org/10.33920/pro-2-2203-03.

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The article gives tips on how to achieve real savings in electricity costs during the operation of an oxygen station, determined by the speed of performance regulation and the launch of cryogenic and adsorption technologies. A comparative analysis of obtaining 40,000 Nm³ /hr of oxygen with a purity of at least 93% and a pressure of 0.5 MPa at the output of the oxygen station with round-the-clock and year-round operation was carried out. The optimal solution to the problem under consideration is the use of cryogenic technology. The advantage of adsorption technology, compared to cryogenic one,

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Phong, Cu Xuan, Nguyen Quoc Q., and Cu Xuan Cu Xuan P. "Early-Stage Analysis of Air Independent Propulsion Based on Fuel Cells for Small Submarines." Advances in Military Technology 17, no. 2 (2022): 457–69. http://dx.doi.org/10.3849/aimt.01744.

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This paper presents an analysis of the results of a hybrid air independent propulsion based on fuel cells for small submarines. The weight and volume of the investigated propulsion, and the major tactical and technical characteristics of the 540-tonne submarine equipped with this propulsion have been determined. Five onboard systems for the hydrogen storage or generation, and the oxygen storage are considered. Combining a micro-balloon hydrogen system with the cryogenic oxygen storage is the best solution for the propulsion. The submerged endurance and range improved 32.1-64.8 times, as compar

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Klebleev, T. I., and V. Yu Semenov. "Experimental Study of Heat Transfer in the Interwall Space of a Cryogenic Tank with Powder Insulation." Herald of the Bauman Moscow State Technical University. Series Mechanical Engineering, no. 3 (146) (September 2023): 113–26. http://dx.doi.org/10.18698/0236-3941-2023-3-113-126.

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Currently, double-wall cryogenic non-isothermal tanks with vacuum-powder or vacuum-multilayer insulation are used in storage and transportation of such cryogenic liquids as liquid nitrogen, oxygen and liquefied natural gas. If the inner vessel is disrupted, the liquid spills into the heat-insulating space and evaporates as a result of heat inflow from the environment. This increases pressure in the thermal insulation space. To ensure functioning of the tank, it is necessary to limit pressure increase in the heat-insulating space. Results of experiments on evaporation of the liquid nitrogen ent

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Orozco, Salvador, Cynthia L. Ramirez Zamora, Md Amzad Hossain, and Ahsan Choudhuri. "FEA-Based Thermo-Structural Modeling of Cryogenic Storage Tanks in Liquid Propulsion Systems." Aerospace 12, no. 6 (2025): 479. https://doi.org/10.3390/aerospace12060479.

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This investigation presents the comprehensive thermo-structural analysis of the propellant tanks utilized in the CROME propulsion system, focused on examining the structural effects caused by the storage of liquid nitrogen, liquid oxygen, and liquid methane. These fluids operate at extremely low temperatures and generate large thermal stress gradients in the tanks, significantly influencing their structural properties. For this reason, it is of vital importance to inspect the generation of mechanical and thermal stresses in the tanks to assess the risk of structural failure. To accomplish this

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Liang, Wenqing, Zhiyong Shu, Fuming Lu, Yong Wang, Xiaohong Zheng, and Hua Qian. "Study on Interparticle Interaction Force Model to Correct Saturation Density of Real Cryogenic Fluid for LBM Simulation." Sustainability 14, no. 12 (2022): 7414. http://dx.doi.org/10.3390/su14127414.

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Cryogenic liquefaction energy storage is an important form of storage for sustainable energy liquid hydrogen and other gases. The weighting parameter A in the parameter-adjusted two-phase LBM model is important for the deviation of simulation results. The aim of this paper is to discover the appropriate parameter to eliminate the deviation, and to solve the problem of large deviation between the theoretical solution and the simulated value that is caused by using different equations of state in LBM simulation. The modified PT equation of state, which is suitable for cryogenic fluids, is combin

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Rozprawy doktorskie na temat "Cryogenic oxygen storage"

Ford, Mark. "Long term storage and usage of cryogenic propellants for a manned Mars mission." Thesis, Cranfield University, 1996. http://dspace.lib.cranfield.ac.uk/handle/1826/11405.

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The research is concerned with investigating the storage and usage of liquid Hydrogen and Oxygen over a long duration. For this purpose a mission was defined where these two propellants are used to transport a six man crew to Mars and back. The mission duration is a total of 972 days in length with a stopover time at Mars of 454 days. A baseline spacecraft is designed. The two driving philosophies behind the design are reliability and reusability. This baseline spacecraft design was used a a basis for analysing the extreme thermal environment and its impact on the propellant storage temperatur

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Książki na temat "Cryogenic oxygen storage"

Timothy, Martin, Hodgson Ed, and United States. National Aeronautics and Space Administration., eds. Extended mobility unit subcritical liquid oxygen storage and supply system (EMU SLOSSS): Conceptual design study report. Martin Marietta, Civil Space and Communications Company, 1992.

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Rivers, H. Kevin. Cyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept. National Aeronautics and Space Administration, Langley Research Center, 1999.

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Center, Langley Research, ed. Cyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept. National Aeronautics and Space Administration, Langley Research Center, 1999.

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Center, Langley Research, ed. Cyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept. National Aeronautics and Space Administration, Langley Research Center, 1999.

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Center, Langley Research, ed. Cyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept. National Aeronautics and Space Administration, Langley Research Center, 1999.

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George C. Marshall Space Flight Center., ed. STS propellant densification feasibility study data book. National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1994.

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Cyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept. National Aeronautics and Space Administration, Langley Research Center, 1999.

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STS propellant densification feasibility study data book. National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1994.

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Części książek na temat "Cryogenic oxygen storage"

Dutta, Jojit, and Achintya Mukhopadhyay. "Thermodynamic Model of Storage and Discharge of Liquid Hydrogen and Oxygen in Pressure Vessels Under Cryogenic Conditions." In Lecture Notes in Mechanical Engineering. Springer Nature Singapore, 2024. https://doi.org/10.1007/978-981-97-7308-4_13.

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White, Guy K., and Philip J. Meeson. "Storage and handling of liquefied gases." In Experimental Techniques in Low-Temperature Physics. Oxford University PressOxford, 2002. http://dx.doi.org/10.1093/oso/9780198514282.003.0005.

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Abstract It is a question of taste or age whether you use the term ‘dewar’ or not for storage vessels made of various materials and of various shapes. Whatever the case we should remember the seminal contribution of Sir James Dewar in 1898 with his evacuated and silvered glass vessel. This allowed him to produce a visible quantity of liquid hydrogen for the first time. It still seems appropriate to call glass cryogen containers ‘dewars’ but for metal and plastic containers it is a matter of choice. Efficient long-term storage has always been important for liquid oxygen on the industrial scale.

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Streszczenia konferencji na temat "Cryogenic oxygen storage"

Rehman, Wajiha, Muhammad Farhan, and Fatima Rehman. "A Review of Cryogenics Applications for Power and Energy." In ASME 2020 Power Conference collocated with the 2020 International Conference on Nuclear Engineering. American Society of Mechanical Engineers, 2020. http://dx.doi.org/10.1115/power2020-16911.

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Abstract Cryogenic technologies use cryogens such as natural gas, nitrogen, helium, hydrogen, argon, and oxygen as main working fluids. These cryogenic technologies and cryogens are emerging in the fields of energy storage, power generation, and eco-friendly fuels. Recently, researchers have proposed to integrate cryogenic systems with power generation systems including Nuclear power plants and wind turbines, to store surplus energy during the off-peak hours and use it during peak hours. The basic idea is to convert air or some other cryogen into liquid during the off-peak hours and expand it

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Segado, M. A., C. L. Hannon, J. G. Brisson, and J. G. Weisend. "COLLINS CRYOCOOLER DESIGN FOR ZERO-BOIL-OFF STORAGE OF LIQUID HYDROGEN AND OXYGEN IN SPACE." In TRANSACTIONS OF THE CRYOGENIC ENGINEERING CONFERENCE—CEC: Advances in Cryogenic Engineering. AIP, 2010. http://dx.doi.org/10.1063/1.3422310.

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Overbeeke, Arend, Edward Hodgson, Heather L. Paul, Harold Gier, and Lawrence H. Gill. "Prototype Cryogenic Oxygen Storage and Delivery Subsystem for Advanced Spacesuits." In International Conference On Environmental Systems. SAE International, 2007. http://dx.doi.org/10.4271/2007-01-3276.

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Zhou, Lei, J. S. Kapat, L. C. Chow, and S. Y. Lei. "Design of a High Performance Cryocooler for Propellant Liquefaction and Storage on Mars." In ASME 2000 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2000. http://dx.doi.org/10.1115/imece2000-1444.

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Abstract Human exploration of space is extending beyond low earth orbit and Moon as NASA is planning a human mission to Mars in 2014. Past studies indicate that In Situ Propellant Production (ISPP) on Mars is a key enabling technology in Mission to Mars. In ISPP, oxygen and methane, which are to be used as cryogenic propellants for any return vehicle from Mars to Earth, are produced on the Martian surface. Once the propellants are produced in gaseous state, they must be liquefied for storage and use in the ascent vehicle. Cryogenic cooling is needed for both liquefaction and storage since the

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Thibault, J.-P., C. Corre, L. Demeure, and S. Mer. "Thermodynamic Control Systems for Cryogenic Propellant Storage During Long Missions." In ASME 2014 4th Joint US-European Fluids Engineering Division Summer Meeting collocated with the ASME 2014 12th International Conference on Nanochannels, Microchannels, and Minichannels. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/fedsm2014-22217.

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One of the key problems for space launcher, in the context of long duration missions using cryotechnic propulsion, is the pressure rise of the propellant tank due to residual thermal inputs (solar fluxes, mechanical connexions). In order to control self-pressurization and as an alternative to simple but propellant-consuming direct venting (DV) systems, a concept of thermodynamic venting systems (TVS) is considered. The main objective of the TVS concept is to control pressurization with a minimum penalty in mass and propellant losses. The present work combines 0-dimensional modelling and labora

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Moore, J. Jeffrey, Owen Pryor, Ian Cormier, and Jeremy Fetvedt. "Oxygen Storage Incorporated Into Net Power and the Allam-Fetvedt Oxy-Fuel sCO2 Power Cycle – Technoeconomic Analysis." In ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2022. http://dx.doi.org/10.1115/gt2022-82060.

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Abstract With the planned future reliance on variable renewable energy, the ability to store energy for prolonged time periods will be required to reduce the disruption of market fluctuations. This paper presents a method to analyze a hybrid liquid-oxygen (LOx) storage / direct-fired sCO2 power cycle and optimize the economic performance over a diverse range of scenarios. The system utilizes a modified version of the NET Power process to produce energy when energy demand exceeds the supply while displacing much of the cost of the ASU energy requirements through cryogenic storage of oxygen. The

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Ju, Shuai, and Haifeng Zhang. "Langasite Cryogenic Pressure Sensor for Space Shuttle Fuel Tank Monitoring." In ASME 2025 Aerospace Structures, Structural Dynamics, and Materials Conference. American Society of Mechanical Engineers, 2025. https://doi.org/10.1115/ssdm2025-152552.

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Abstract With the increasing demand for outer space exploration, particularly for NASA missions, the structural safety of space shuttles has garnered significant attention over the past decades. One critical aspect is the external fuel tank, which stores liquid hydrogen and oxygen at cryogenic temperatures of −253°C and −183°C, respectively. Detecting early-stage changes in temperature or pressure is crucial for preventing serious issues in fuel storage or even catastrophic failures in the spacecraft. Accurate and frequent pressure monitoring within the fuel tanks is essential to avoid malfunc

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Shelby, Jason L., and Krishna Kota. "Design of a High-Effective Wavy Channel Heat Exchanger for Cryogenic Applications." In ASME 2015 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/imece2015-52833.

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Long duration thermal control of cryogenic propellants is a high priority mission activity for NASA. A 20 K cryocooler capable of 20 W of refrigeration would offer a significant mass savings in cryogen storage by facilitating propellant zero boil-off and hence long term cryogen storage, which would provide scope for long duration missions beyond low Earth orbit (LEO). For direct current (DC) type cryocoolers, as well as open cycle liquefaction systems, effective recuperative heat exchange is a highly critical function. Coefficient of Performance (COP) of cryocoolers is greatly sensitive to hea

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Notardonato, W., G. Haddad, K. V. Krishna-Murty, J. Zhu, J. S. Kapat, and L. C. Chow. "Miniature Joule–Thomson (JT) Cryocoolers for Propellant Management." In ASME 2004 International Mechanical Engineering Congress and Exposition. ASMEDC, 2004. http://dx.doi.org/10.1115/imece2004-61545.

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Boil-off of cryogenic propellants is an issue of concern in any space mission. There could be boil-off of liquid propellants in the cryogenic storage tank, transfer line or in the space vehicle external tank itself due to heat leak. The current insulation technology uses a multilayered thermal protective coating of 304 Stainless Steel and Welded Invar, which allows the propellant to withstand the extreme internal and external temperature variations generated during pre-launch, launch, and flight operations, which does not provide for zero boil-off (ZBO). Usage of a cryocooler to prevent propel

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Sander, Frank, Sebastian Foeste, and Roland Span. "Model of an Oxygen Transport Membrane for Coal Fired Power Cycles With CO2 Capture." In ASME Turbo Expo 2007: Power for Land, Sea, and Air. ASMEDC, 2007. http://dx.doi.org/10.1115/gt2007-27788.

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Greenhouse gas emissions from power generation will increase in future if the demand for electrical energy does not subside. Therefore capture and storage of carbon dioxide (CO2) will become important technologies for lowering the rate of increase of global CO2 emissions, or even reducing them. A promising technology for coal fired power cycles is the integrated gasification combined cycle (IGCC), where CO2 is separated from the syngas coming from the gasifier before the syngas is combusted in a more or less conventional gas turbine. But oxygen is required for the gasification process to achie

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