Relevant bibliographies by topics / Modular propulsion system

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  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Modular propulsion system'

Author: Grafiati
Published: 4 June 2021
Last updated: 9 February 2022

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Journal articles on the topic "Modular propulsion system"

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Yan, Zheng, Xiao Hui Peng, Yu Qiang Cheng, and Jian Jun Wu. "Modeling and Simulation of System Dynamics for Spacecraft Propulsion System." Applied Mechanics and Materials 229-231 (November 2012): 2112–16. http://dx.doi.org/10.4028/www.scientific.net/amm.229-231.2112.

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The spacecraft propulsion system is used for geosynchronous orbit transfer, three-axis stabilization and station-keeping. In order to investigate the system dynamics of spacecraft propulsion system with complex pressurization pipelines and propellant supply pipelines, a modular and extensible simulator UPSSim was developed. The pressurant pipelines were separated into several nodes, each node used lumped parameter model; while the propellant feed pipelines used distributed parameter model. Heat transfer between components and environment was also taken into account. The model accurately predic
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Igenbergs, E., and M. Kirschner. "A modular propulsion system for the interorbital vehicle." Acta Astronautica 15, no. 8 (1987): 545–50. http://dx.doi.org/10.1016/0094-5765(87)90154-8.

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Adami, Amirhossein, Mahda Mortazavi, and Mehran Nosratollahi. "Multi-modular design optimization and multidisciplinary design optimization." International Journal of Intelligent Unmanned Systems 3, no. 2/3 (2015): 156–70. http://dx.doi.org/10.1108/ijius-01-2015-0001.

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Purpose – For complex engineering problems, multidisciplinary design optimization (MDO) techniques use some disciplines that need to be run several times in different modules. In addition, mathematical modeling of a discipline can be improved for each module. The purpose of this paper is to show that multi-modular design optimization (MMO) improves the design performances in comparison with MDO technique for complex systems. Design/methodology/approach – MDO framework and MMO framework are developed to optimum design of a complex system. The nonlinear equality and inequality constrains are con
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Yan, Zheng, Xiao Hui Peng, Yu Qiang Cheng, and Jian Jun Wu. "System Dynamic Characteristic Simulation of Spacecraft Propulsion System Based on AMESim." Advanced Materials Research 605-607 (December 2012): 679–83. http://dx.doi.org/10.4028/www.scientific.net/amr.605-607.679.

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In order to investigate the dynamic characteristic of the spacecraft propulsion system, numerical simulation was carried out based on the modular and extensible simulation model UPSSim. The model accurately predicts the global behavior of the spacecraft propulsion system in the priming and shutdown process, and also correctly describes the transient behavior of the subsystems. Due to the distributaries of the attitude control thruster supply pipelines, the propellant flow fluctuation attenuates rapidly in the priming process and the waterhammer peak pressure of main engine supply pipelines dec
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Campora, U., and M. Figari. "Numerical simulation of ship propulsion transients and full-scale validation." Proceedings of the Institution of Mechanical Engineers, Part M: Journal of Engineering for the Maritime Environment 217, no. 1 (2003): 41–52. http://dx.doi.org/10.1243/147509003321623130.

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The paper describes a mathematical model for the dynamics simulation of ship propulsion systems. The model, developed in a MATLAB-SIMULINK software environment, is structured in modular form; the various elements of the system are described as individuals blocks (hull, prime mover, gear, waterjet, etc.) and linked together to take their interactions into account. In this way it is possible to characterize the dynamic behaviour of both the single component and the whole propulsion plant. The model may be used to analyse the system response at off-design and transient conditions. In particular,
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Nosseir, Ahmed E. S., Angelo Cervone, and Angelo Pasini. "Modular Impulsive Green Monopropellant Propulsion System (MIMPS-G): For CubeSats in LEO and to the Moon." Aerospace 8, no. 6 (2021): 169. http://dx.doi.org/10.3390/aerospace8060169.

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Green propellants are currently considered as enabling technology that is revolutionizing the development of high-performance space propulsion, especially for small-sized spacecraft. Modern space missions, either in LEO or interplanetary, require relatively high-thrust and impulsive capabilities to provide better control on the spacecraft, and to overcome the growing challenges, particularly related to overcrowded LEOs, and to modern space application orbital maneuver requirements. Green monopropellants are gaining momentum in the design and development of small and modular liquid propulsion s
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Xiao, Nengqi, Ruiping Zhou, and Xiang Xu. "Vibration of diesel-electric hybrid propulsion system with nonlinear component." Journal of Vibration and Control 24, no. 22 (2018): 5353–65. http://dx.doi.org/10.1177/1077546317753010.

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The lumped parameter method is used to model the components of a marine diesel-electric hybrid propulsion system. Modular modeling and five basic models of torsional vibration are used to establish the torsion of the diesel-electric hybrid propulsion system with a nonlinear components vibration mathematical model. In order to include the nonlinear parts of the marine diesel-hybrid propulsion shafting torsional vibration system characteristics, by combining the perturbation method with the advantages and disadvantages of the harmonic method, a perturbation-harmonic method is presented to solve
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Cui, Ze, Zeng Jun Han, Hong Wei Pan, Yao Hua Wang, and Xiao Qing Hua. "The Optimization Design of a Propulsion Module for a Mini-ROV." Advanced Materials Research 403-408 (November 2011): 2795–99. http://dx.doi.org/10.4028/www.scientific.net/amr.403-408.2795.

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For a mini remotely operated vehicle (mini-ROV), the performance of the propulsion system has a direct impact on its underwater running and operation. A proper designed propulsion module will improve the maneuverability and controllablity of the mini ROV. In this paper, we propose a kind of propulsion modular series taking lower drag, higher efficiency and lighter weight as design objectives. Simulation and experiment results are also presented to illustrate performance of a specific designed thruster.
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Matlock, Jay, Stephen Warwick, Philipp Sharikov, Jenner Richards, and Afzal Suleman. "Evaluation of energy efficient propulsion technologies for unmanned aerial vehicles." Transactions of the Canadian Society for Mechanical Engineering 43, no. 4 (2019): 481–89. http://dx.doi.org/10.1139/tcsme-2018-0231.

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The transition to cleaner, more efficient and longer-endurance aircraft is at the forefront of research and development in air vehicles. The focus of this research is to experimentally evaluate hybrid propulsion and energy harvesting systems in unmanned aerial vehicles (UAVs). Hybrid systems offer benefits over conventional gasoline and electric systems including lower environmental impacts, reduced fuel consumption, redundancy, and distributed propulsion. Additional energy efficiency can be achieved by harvesting some of the thermal energy of the exhaust gases. The development and experimenta
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Machado, Leonardo, Jay Matlock, and Afzal Suleman. "Experimental evaluation of a hybrid electric propulsion system for small UAVs." Aircraft Engineering and Aerospace Technology 92, no. 5 (2019): 727–36. http://dx.doi.org/10.1108/aeat-06-2019-0120.

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Purpose This paper aims to experimentally evaluate the performance of a parallel hybrid propulsion system for use in small unmanned aerial vehicles (UAVs). Design/methodology/approach The objective is to combine all the individual components of the hybrid electric propulsion system (HEPS) into a modular test bench to characterize the performance of a parallel hybrid propulsion system, and to evaluate a rule-based controller based on the ideal operating line concept for the control of the power plant. Electric motor (EM) designed to supplement the power of the internal combustion engine (ICE) t
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Dissertations / Theses on the topic "Modular propulsion system"

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Skendraoui, Nadir. "FAUTEUIL ROULANT MANUEL OPTIMISE ET MODULABLE." Thesis, Reims, 2020. http://www.theses.fr/2020REIMS018.

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Le fauteuil roulant manuel (FRM) fait partie de la vie quotidienne des personnes atteintes d’handicape moteur. L’objectif de cette thèse est de développer un nouveau FRM basé sur une approche mécanique qui permet de quantifier les efforts résistants dans le but final de concevoir un nouveau système de propulsion manuel modulable qui équipera le FRM. L’approche mécanique fait intervenir plusieurs paramètres cinématiques (vitesse, accélération…) et dynamiques (force de propulsion, résistance au roulement, résistance de l’air…) pour quantifier la charge résistante qui sera par la suite utilisé po
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Sarar, Stephen F. "A galvanically isolated power converter module for DC Zonal Electric Distribution Systems." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2006. http://library.nps.navy.mil/uhtbin/hyperion/06Mar%5FSarar.pdf.

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Thesis (M.S. in Electrical Engineering)--Naval Postgraduate School, March 2006.<br>Thesis Advisor(s): Robert W. Ashton, Andrew A. Parker. "March 2006." Includes bibliographical references (p. 73). Also available online.
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Nelms, Robert Mark. "Simulation of spacecraft power systems using a modular state variable approach." Diss., Virginia Polytechnic Institute and State University, 1987. http://hdl.handle.net/10919/53653.

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The power requirements for future spacecraft power systems will be on the order of a few hundred kilowatts to a few megawatts. Because of these power levels, a high-voltage, high-power distribution subsystem may be utilized to transmit power from the source to the different loads. Using current state-of-the-art power conditioning electronics, complex series and parallel configurations will be required at the interface between the source and the distribution subsystem and between the distribution subsystem and the loads. The dynamic response of such a spacecraft power system may be obtained u
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Flath, Allen III. "Mathematical Programming Approach for the Design of Satellite Power Systems." UKnowledge, 2019. https://uknowledge.uky.edu/ece_etds/136.

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Satellite power systems can be understood as islanded dc microgrids supplied by specialized and coordinated solar cell arrays augmented by electrochemical battery systems to handle high-power loads and periods of eclipse. The periodic availability of power, the limited capacity of batteries, and the dependence of all mission service on power consumption create a unique situation in which temporal power and energy scarcity exist. A multi-period model of an orbital satellite power system’s performance over a mission’s duration can be constructed. A modular power system architecture is used to ch
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Books on the topic "Modular propulsion system"

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L, Felder James, and United States. National Aeronautics and Space Administration., eds. Predicted performance of an integrated modular engine system. National Aeronautics and Space Administration, 1993.

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C, Rapp Douglas, and United States. National Aeronautics and Space Administration., eds. Reliability studies of Integrated modular engine system designs. National Aeronautics and Space Administration, 1993.

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Reliability studies of Integrated modular engine system designs. National Aeronautics and Space Administration, 1993.

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High leverage space transportation system technologies for human exploration missions to the moon and beyond. National Aeronautics and Space Administration, 1996.

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Book chapters on the topic "Modular propulsion system"

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Howe, Steven D. "Advanced Propulsion: Pulsed, Fusion, Antimatter and Breakthrough Physics." In Reference Module in Earth Systems and Environmental Sciences. Elsevier, 2020. http://dx.doi.org/10.1016/b978-0-12-819725-7.00022-2.

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Conference papers on the topic "Modular propulsion system"

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Nelson, Steven D., and Peter Current. "Modular Architecture Propulsion System (MAPS™)." In 2018 Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-4704.

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EMERICK, ROGER, and JAMES O'COIN. "A modular propulsion system for missile attitude control." In 25th Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-2952.

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MORANO, JOSEPH, and JOHN HENDERSON. "A modular propulsion system required for Space Station assembly." In 25th Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-2613.

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Sievers, Robert K., Thomas K. Hunt, Joseph F. Ivanenok, Jan E. Pantolin, and David A. Butkiewicz. "Modular radioisotope AMTEC power system." In Proceedings of the tenth symposium on space nuclear power and propulsion. AIP, 1993. http://dx.doi.org/10.1063/1.43168.

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HARDY, TERRY, and DOUGLAS RAPP. "Reliability studies of Integrated Modular Engine system designs." In 29th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-1886.

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FRANKENFIELD, BRUCE, and JERRY CAREK. "Fluid design studies of integrated modular engine system." In 29th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-1887.

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BINDER, MICHAEL, and JAMES FELDER. "Predicted performance of an Integrated Modular Engine system." In 29th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-1888.

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HOBBS, L. "The design of a general purpose modular propellant feed system." In 26th Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-1939.

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Allotta, Benedetto, Riccardo Costanzi, Jonathan Gelli, Luca Pugi, and Alessandro Ridolfi. "Design of a modular propulsion system for MARTA AUV." In OCEANS 2015 - Genova. IEEE, 2015. http://dx.doi.org/10.1109/oceans-genova.2015.7271397.

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Spichartz, M., V. Staudt, and A. Steimel. "Modular Multilevel Converter for propulsion system of electric ships." In 2013 IEEE Electric Ship Technologies Symposium (ESTS 2013). IEEE, 2013. http://dx.doi.org/10.1109/ests.2013.6523740.

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Reports on the topic "Modular propulsion system"

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Kelly, K., J. Brown, G. Kamsickas, and W. Tucker. Modular Simulator System (MSS). System/Segment Specification for the Generic Modular Simulator System - Propulsion Module Propulsion Module. Volume 5. Defense Technical Information Center, 1993. http://dx.doi.org/10.21236/ada276972.

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