Relevant bibliographies by topics / Propulsion systems design

Contents

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

Academic literature on the topic 'Propulsion systems design'

Author: Grafiati
Published: 4 June 2021
Last updated: 1 February 2022

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Journal articles on the topic "Propulsion systems design"

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Dimitrova, Zlatina. "Vehicle propulsion systems design methods." MATEC Web of Conferences 133 (2017): 02001. http://dx.doi.org/10.1051/matecconf/201713302001.

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Blount, Donald L., and Robert J. Bartee. "Design of Propulsion Systems for High-Speed Craft." Marine Technology and SNAME News 34, no. 04 (October 1, 1997): 276–92. http://dx.doi.org/10.5957/mt1.1997.34.4.276.

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The demand for increased speed in medium and large craft challenges the designer to select propulsion systems which meet performance requirements economically throughout ever-widening operational profiles. The combined hydrodynamic characteristics of hull and propulsors result in a speed-thrust relationship for the environment in which the vessel operates. This speed-thrust relationship requires unique values of power and RPM input for each type and number of propulsors. Power and RPM are also sensitive to the mode of operation of the vessel whether at constant speed, accelerating to a greater speed or towing an object. Most vessels utilize fixed-pitch submerged propellers. Surface propellers are fitted to vessels designed to perform at very high speeds and waterjetpropulsors are being utilized with increasing frequency on larger vessels with high-speed operational profile. This paper discusses brake horsepower (BHP) and propulsor RPM relationships for vessel speed requirements based on the hydrodynamic characteristics of three types of propulsors: submerged propellers, surface propellers and waterjets. An example of predicted vessel performance regarding speed, power and propulsor RPM is presented which includes engine characteristics and BHP versus RPM. This latter format depicts the differences in power demand for three types of propulsors on a monohull vessel with regard to engine characteristics.
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POYRAZ, Özgür, and Melih Cemal KUŞHAN. "DESIGN FOR ADDITIVE MANUFACTURING WITH CASE STUDIES ON AIRCRAFTS AND PROPULSION SYSTEMS." SCIENTIFIC RESEARCH AND EDUCATION IN THE AIR FORCE 21, no. 1 (October 8, 2019): 166–75. http://dx.doi.org/10.19062/2247-3173.2019.21.23.

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Gagarinov, I. "Structures of high-power electric propulsion systems." Transactions of the Krylov State Research Centre 1, no. 395 (March 9, 2021): 119–31. http://dx.doi.org/10.24937/2542-2324-2021-1-395-119-131.

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Object and purpose of research. This paper discusses structures of high-power electric propulsion systems for ships. The purpose was to give a summary of design solutions made in development of these systems. Materials and methods. This paper relies on academic and technical data, as well on the long-term author’s experience in marine electric propulsion R&Ds. The solution suggested by the author is based on the comparative analysis of design solutions adopted in the development of structures for high-power marine electric power and propulsion systems. Main results. Summary on design solutions for high-power electric propulsion systems of such ships as icebreakers, oil tankers, LNGCs and cruise liners. Conclusion. Results obtained by author were used in the design of the electric propulsion system of the «Lider» nuclear icebreaker and further could be used in design of Arctic vessels.
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Kaul, Stefan, Paul Mertes, and Lutz Müller. "Application-optimised propulsion systems for energy-efficient operation." Ciencia y tecnología de buques 5, no. 9 (July 23, 2011): 87. http://dx.doi.org/10.25043/19098642.53.

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Today, optimal propellers are designed by using advanced numerical methods. Major revolutionary improvements cannot be expected. More essential are the design conditions and the optimal adaptation of the propulsion system according to the operational requirements. The selection and optimisation of the propulsion system based on a systematic analysis of the ship’s requirements and the operation profile are the prerequisites for reliable and energy-efficient propulsion. Solutions are presented, which accommodate these issues with a focus on steerable rudderpropellers. Considerations include the efficiency potential of the propulsor itself, optimisation of the engine propeller interaction, and optimisation of a demandresponsive energy supply. The propeller-thruster interaction is complex, but offers some potential for optimisation. Results of examinations show this. The power distribution between multiple propellers at high loads of limited propeller diameters increases the efficiency. This can be done by double-propeller systems like the SCHOTTEL TwinPropeller or by distributing the power on several thrusters. This distributed propulsion offers economic operation and an increased lifetime by means of the demandresponsive use of energy. An efficiency-optimized electric motor instead of the upper gear box reduces the mechanical losses in the case of diesel-electric propulsion. An example: the SCHOTTEL CombiDrive.
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Leśniewski, Wojciech, Daniel Piątek, Konrad Marszałkowski, and Wojciech Litwin. "Small Vessel with Inboard Engine Retrofitting Concepts; Real Boat Tests, Laboratory Hybrid Drive Tests and Theoretical Studies." Energies 13, no. 10 (May 20, 2020): 2586. http://dx.doi.org/10.3390/en13102586.

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The development of modern technologies and their increasing availability, as well as the falling costs of highly efficient propulsion systems and power sources, have resulted in electric or hybrid propulsions systems’ growing popularity for use on watercraft. Presented in the paper are design and lab tests of a prototype parallel hybrid propulsion system. It describes a concept of retrofitting a conventionally powered nine meter-long vessel with the system, and includes results of power and efficiency measurements, as well as calculations of the vessel’s operating range under the propulsion of its electric motor. The concept of adding of a solar panels array was studied.
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Dahms, Julius, and Andreas Bardenhagen. "Propulsion model for (hybrid) unmanned aircraft systems (UAS)." Aircraft Engineering and Aerospace Technology 91, no. 2 (February 4, 2019): 373–80. http://dx.doi.org/10.1108/aeat-01-2018-0033.

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Purpose This paper deals with the estimation of the necessary masses of propulsion components for multirotor UAS. Originally, within the design process of multirotors, this is an iterative problem, as the propulsion masses contribute to the total takeoff mass. Hence, they influence themselves and cannot be directly calculated. The paper aims to estimate the needed propulsion masses with respect to the requested thrust because of payload, airframe weight and drag forces and with respect to the requested flight time. Design/methodology/approach Analogue to the well-established design synthesis of airplanes, statistical data of existing electrical motors, propellers and rechargeable batteries are evaluated and analyzed. Applying Rankine and Froude’s momentum theory and a generic model for electro motor efficiency factors on the statistical performance data provides correlations between requested performance and, therefore, needed propulsion masses. These correlations are evaluated and analyzed in the scope of buoyant-vertical-thrusted hybrid UAS. Findings This paper provides a generic mathematical propulsion model. For given payloads, airframe structure weights and a requested flight time, appropriate motor, propeller and battery masses can be modelled that will provide appropriate thrust to lift payload, airframe and the propulsion unit itself over a requested flight time. Research limitations/implications The model takes into account a number of motors of four and is valid for the category of nano and small UAS. Practical implications The presented propulsion model enables a full numerical design process for vertical thrusted UAS. Hence, it is the precondition for design optimization and more efficient UAS. Originality/value The propulsion model is unique and it is valid for pure multirotor as well as for hybrid UAS too.
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Jahshan, S. N., and T. Kammash. "Multimegawatt Nuclear Reactor Design for Plasma Propulsion Systems." Journal of Propulsion and Power 21, no. 3 (May 2005): 385–91. http://dx.doi.org/10.2514/1.5456.

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MISHIO, Ryoichi, and Tadashi KASHIMA. "Design of Optimal Feedback Control for Propulsion Systems." Proceedings of Conference of Kansai Branch 2003.78 (2003): _12–15_—_12–16_. http://dx.doi.org/10.1299/jsmekansai.2003.78._12-15_.

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Islam, Mohammed F., Brian Veitch, Neil Bose, and Pengfei Liu. "Numerical Study of Hub Taper Angle on Podded Propeller Performance." Marine Technology and SNAME News 43, no. 01 (January 1, 2006): 1–10. http://dx.doi.org/10.5957/mt1.2006.43.1.1.

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Presently, the majority of podded propulsion systems are of the pulling type, because this type provides better hydrodynamic efficiency than the pushing type. There are several possible explanations for the better overall performance of a puller-type podded propulsor. One is related to the difference in hub taper angle. Puller and pusher propellers have opposite hub taper angles, hence different hub and blade root shape. These differences cause changes in the flow condition and possibly influence the overall performance. The current study focuses on the variation in performance of pusher and puller propellers with the same design of blade sections, but different hub taper angles. A hyperboloidal low-order source-doublet steady/unsteady time domain panel method code, PROPELLA, was modified and used to evaluate effects of hub taper angle on the open water propulsive performance of some fixed-pitch screw propellers used in podded propulsion systems. Major findings include good agreement between predictions using the modified code and measurements, significant effects of hub taper angle on propulsive performance of tapered hub propellers, and noticeable effects of hub taper angle on sectional pressure distributions of tapered hub propeller blades.
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Dissertations / Theses on the topic "Propulsion systems design"

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Ballard, Michael A. "Impacts of electric propulsion systems on submarine design." Thesis, Springfield, Va. : Available from the National Technical Information Service, 1989. http://handle.dtic.mil/100.2/ADA213542.

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Thesis (Degree of Naval Engineer and M.S. in Electrical Engineering and Computer Science) Massachusetts Institute of Technology, June 1989.
Includes bibliographical references. Also available online.
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Leonessa, Alexander. "Hierarchical robust nonlinear switching control design for propulsion systems." Diss., Georgia Institute of Technology, 1999. http://hdl.handle.net/1853/11997.

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Björk, Daniel. "Automated Propulsion Kit Selection for MAV : A Design Process Tool." Thesis, Linköping University, Department of Mechanical Engineering, 2004. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-4164.

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This thesis project has been carried out at Linköpings universitet at the Department of Mechanical Engineering. The emphasis of the project lies in the exploration of automatic selection of components for a propulsion kit. Specifically for this project, propulsion based on electric power and meeting the requirements for use in a Micro Aerial Vehicle (MAV). The key features include a systematic selection method based on user criterias and a model for evaluating propeller performance. These are implemented in a program written as a part of the project. The conclusion is that it is possible to make a program capable of a component selection and that the programs usability is mainly reliant on three factors: model for propeller evaluation, method of selection and the quality of the component database.

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Hall, Philip D. "Design of a coaxial split flow pulse detonation engine." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2006. http://library.nps.navy.mil/uhtbin/hyperion/06Jun%5FHall.pdf.

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Thesis (M.S. in Mechanical Engineering)--Naval Postgraduate School, June 2006.
Thesis Advisor(s): Jose O. Sinibaldi, Christopher M. Brophy. "June 2006." Includes bibliographical references (p. 41-42). Also available in print.
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Bradford, John Edward. "A technique for rapid prediction of aftbody nozzle performance for hypersonic launch vehicle design." Diss., Georgia Institute of Technology, 2001. http://hdl.handle.net/1853/12896.

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Kwon, Kybeom. "A novel numerical analysis of Hall Effect Thruster and its application in simultaneous design of thruster and optimal low-thrust trajectory." Diss., Georgia Institute of Technology, 2010. http://hdl.handle.net/1853/34777.

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Hall Effect Thrusters (HETs) are a form of electric propulsion device which uses external electrical energy to produce thrust. When compared to various other electric propulsion devices, HETs are excellent candidates for future orbit transfer and interplanetary missions due to their relatively simple configuration, moderate thrust capability, higher thrust to power ratio, and lower thruster mass to power ratio. Due to the short history of HETs, the current design process of a new HET is a largely empirical and experimental science, and this has resulted in previous designs being developed in a narrow design space based on experimental data without systematic investigations of parameter correlations. In addition, current preliminary low-thrust trajectory optimizations, due to inherent difficulties in solution procedure, often assume constant or linear performances with available power in their applications of electric thrusters. The main obstacles come from the complex physics involved in HET technology and relatively small amounts of experimental data. Although physical theories and numerical simulations can provide a valuable tool for design space exploration at the inception of a new HET design and preliminary low-thrust trajectory optimization, the complex physics makes theoretical and numerical solutions difficult to obtain. Numerical implementations have been quite extensively conducted in the last two decades. An investigation of current methodologies reveals that to date, none provide a proper methodology for a new HET design at the conceptual design stage and the coupled low-thrust trajectory optimization. Thus, in the first half of this work, an efficient, robust, and self-consistent numerical method for the analysis of HETs is developed with a new approach. The key idea is to divide the analysis region into two regions in terms of electron dynamics based on physical intuition. Intensive validations are conducted for existing HETs from 1 kW to 50 kW classes. The second half of this work aims to construct a simultaneous design optimization environment though collaboration with experts in low-thrust trajectory optimization where a new HET and associated optimal low-thrust trajectory can be designed simultaneously. A demonstration for an orbit raising mission shows that the constructed simultaneous design optimization environment can be used effectively and synergistically for space missions involving HETs. It is expected that the present work will aid and ease the current expensive experimental HET design process and reduce preliminary space mission design cycles involving HETs.
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Cheney, Liam Jon. "Development of Safety Standards for CubeSat Propulsion Systems." DigitalCommons@CalPoly, 2014. https://digitalcommons.calpoly.edu/theses/1180.

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The CubeSat community has begun to develop and implement propulsion systems. This movement represents a new capability which may satisfy mission needs such as orbital and constellation maintenance, formation flight, de-orbit, and even interplanetary travel. With the freedom and capability granted by propulsion systems, CubeSat providers must accept new responsibilities in proportion to the potential hazards that propulsion systems may present. The Cal Poly CubeSat program publishes and maintains the CubeSat Design Specification (CDS). They wish to help the CubeSat community to safety and responsibly expand its capabilities to include propulsive designs. For this reason, the author embarked on the task of developing a draft of safety standards CubeSat propulsion systems. Wherever possible, the standards are based on existing documents. The author provides an overview of certain concepts in systems safety with respect to the classification of hazards, determination of required fault tolerances, and the use of inhibits to satisfy fault tolerance requirements. The author discusses hazards that could exist during ground operations and through launch with respect to hazardous materials and pressure systems. Most of the standards related to Range Safety are drawn from AFSPCMAN 91-710. Having reviewed a range of hypothetical propulsion system architectures with an engineer from Range Safety at Vandenberg Air Force Base, the author compiled a case study. The author discusses many aspects of orbital safety. The author discusses the risk of collision with the host vehicle and with third party satellites along with the trackability of CubeSats using propulsion systems. Some recommendations are given for working with the Joint Functional Component Command for Space (JFCC SPACE), thanks to the input of two engineers who work with the Joint Space Operations Center (JSpOC). Command Security is discussed as an important aspect of a mission which implements a propulsion system. The author also discusses End-of-Life procedures such as safing and de-orbit operations. The orbital safety standards are intended to promote “good citizenship.” The author steps through each proposed standard and offers justification. The author is confident that these standards will set the stage for a dialogue in the CubeSat community which will lead to the formulation of a reasonable and comprehensive set of standards. The author hopes that the discussions given throughout this document will help CubeSat developers to visualize the path to flight readiness so that they can get started on the right foot.
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Rajkumar, Vishnu Ganesh. "Design Optimization of a Regional Transport Aircraft with Hybrid Electric Distributed Propulsion Systems." Thesis, Virginia Tech, 2018. http://hdl.handle.net/10919/84494.

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In recent years, there has been a growing shift in the world towards sustainability. For civil aviation, this is reflected in the goals of several organizations including NASA and ACARE as significantly increased fuel efficiency along with reduced harmful emissions in the atmosphere. Achieving the goals necessitates the advent of novel and radical aircraft technologies, NASA's X-57, is one such concept using distributed electric propulsion (DEP) technology. Although practical implementation of DEP is achievable due to the scale invariance of highly efficient electric motors, the current battery technology restricts its adoption for commercial transport aircraft. A Hybrid Electric Distributed Propulsion (HEDiP) system offers a promising alternative to the all-electric system. It leverages the benefits of DEP when coupled with a hybrid electric system. One of the areas needing improvement in HEDiP aircraft design is the fast and accurate estimation of wing aerodynamic characteristics in the presence of multiple propellers. A VLM based estimation technique was developed to address this requirement. This research is primarily motivated by the need to have mature conceptual design methods for HEDiP aircraft. Therefore, the overall research objective is to develop an effective conceptual design capability based on a proven multidisciplinary design optimization (MDO) framework, and to demonstrate the resulting capability by applying it to the conceptual design of a regional transport aircraft (RTA) with HEDiP systems.
Master of Science
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Roth, Bryce Alexander. "A theoretical treatment of technical risk in modern propulsion system design." Diss., Georgia Institute of Technology, 2000. http://hdl.handle.net/1853/12221.

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Harper, James M. "Pocket Rocket: A 1U+ Propulsion System Design To Enhance CubeSat Capabilities." DigitalCommons@CalPoly, 2020. https://digitalcommons.calpoly.edu/theses/2218.

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The research presented provides an overview of a 1U+ form factor propulsion system design developed for the Cal Poly CubeSat Laboratory (CPCL). This design utilizes a Radiofrequency Electrothermal Thruster (RFET) called Pocket Rocket that can generate 9.30 m/s of delta-V with argon, and 20.2 ± 3 m/s of delta-V with xenon. Due to the demand for advanced mission capabilities in the CubeSat form factor, a need for micro-propulsion systems that can generate between 1 – 1500 m/s of delta-V are necessary. By 2019, Pocket Rocket had been developed to a Technology Readiness Level (TRL) of 5 and ground tested in a 1U CubeSat form factor that incorporated propellant storage, pressure regulation, RF power and thruster control, as well as two Pocket Rocket thrusters under vacuum, and showcased a thrust of 2.4 mN at a required 10 Wdc of power with Argon propellant. The design focused on ground testing of the thruster and did not incorporate all necessary components for operation of the thruster. Therefore in 2020, a 1U+ Propulsion Module that incorporates Pocket Rocket, the RF amplification PCB, a propellant tank, propellant regulation and delivery, as well as a DC-RF conversion with a PIB, that are all attached to a 2U customer CubeSat for a 3U+ overall form factor. This design was created to increase the TRL level of Pocket Rocket from 5 to 8 by demonstrating drag compensation in a 400 km orbit with a delta-V of 20 ± 3 m/s in the flight configuration. The 1U+ Propulsion Module design included interface and requirements definition, assembly instructions, Concept of Operations (ConOps), as well as structural and thermal analysis of the system. The 1U+ design enhances the capabilities of Pocket Rocket in a 1U+ form factor propulsion system and increases future mission capabilities as well as propulsion system heritage for the CPCL.
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Books on the topic "Propulsion systems design"

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

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

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

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

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Weldon, Vincent. Design optimization of gas generator hybrid propulsion boosters. [Washington, DC]: National Aeronautics and Space Administration, 1990.

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

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

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

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

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

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Book chapters on the topic "Propulsion systems design"

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Suresh, B. N., and K. Sivan. "Propulsion Systems." In Integrated Design for Space Transportation System, 329–90. New Delhi: Springer India, 2015. http://dx.doi.org/10.1007/978-81-322-2532-4_9.

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Sackheim, Robert L., Robert S. Wolf, and Sidney Zafran. "Space Propulsion Systems." In Space Mission Analysis and Design, 637–64. Dordrecht: Springer Netherlands, 1992. http://dx.doi.org/10.1007/978-94-011-2692-2_17.

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Sackheim, Robert L., Robert S. Wolf, and Sidney Zafran. "Space Propulsion Systems." In Space Mission Analysis and Design, 579–606. Dordrecht: Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3794-2_17.

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Most, Michael T., and Graham Feasey. "UAS Propulsion System Design." In Introduction to Unmanned Aircraft Systems, 245–66. 3rd ed. Third editon. | Boca Raton: CRC Press, 2021.: CRC Press, 2021. http://dx.doi.org/10.1201/9780429347498-11.

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Sackheim, Robert L., Robert S. Wolf, and Sidney Zafran. "Erratum to: Space Propulsion Systems." In Space Mission Analysis and Design, 874. Dordrecht: Springer Netherlands, 1992. http://dx.doi.org/10.1007/978-94-011-2692-2_27.

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Skendraoui, Nadir, Fabien Bogard, Sébastien Murer, Tareq Z. Ahram, Krzysztof Fiok, and Redha Taiar. "The Musculoskeletal Contribution in Wheelchair Propulsion Systems: Numerical Analysis." In Advances in Ergonomics in Design, 251–60. Cham: Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-94706-8_28.

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Dallagi, Habib, and Bechir Sabri. "State Feedback Control of Ship Electric Propulsion System." In Design and Modeling of Mechanical Systems - II, 221–32. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-17527-0_22.

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Alcoléa, Vitor, Fausto Orsi Medola, Guilherme da Silva Bertolaccini, and Frode Eika Sandnes. "Effect of Added Mass Location on Manual Wheelchair Propulsion Forces." In Human Systems Engineering and Design II, 747–53. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-27928-8_114.

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Dallagi, Habib, Chiheb Zaoui, and Samir Nejim. "Modelization and Multimodel Control of Ship Electric Propulsion System." In Design and Modeling of Mechanical Systems—III, 97–113. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-66697-6_11.

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Chocron, Olivier, and Emmanuel Delaleau. "Trajectory-Based Synthesis of Propulsion Systems for Fixed-Thrusters AUVs." In ROMANSY 22 – Robot Design, Dynamics and Control, 380–91. Cham: Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-78963-7_48.

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Conference papers on the topic "Propulsion systems design"

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HERRICK, P. "Fighter aircraft/propulsion integration." In Aircraft Systems, Design and Technology Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-2658.

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INOUE, TOSHIAKI, JUN-ICHI HIROKAWA, TOSHIO HANAI, and HIKARU TAKAMI. "Conceptual study of supersonic propulsion systems." In Aircraft Design and Operations Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-3133.

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BROOKS, A. "Propulsion systems for vertical flight aircraft." In Aircraft Design, Systems and Operations Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-3299.

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ADAMSON, A., and A. STUART. "Propulsion for advanced commercial transports." In Aircraft Design Systems and Operations Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1985. http://dx.doi.org/10.2514/6.1985-3061.

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COONS, L. "Propulsion challenges for hypersonic flight." In Aircraft Systems, Design and Technology Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-2620.

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Owen, David. "APOLLO SPACECRAFT PROPULSION SYSTEMS DESIGN PHILOSOPHIES." In AIAA SPACE 2010 Conference & Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-8813.

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WIDDISION, C., E. SCHREFFLER, and C. HOSKING. "Aircraft synthesis with propulsion installation effects." In Aircraft Design, Systems and Operations Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-4404.

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CHAMIS, C., and S. SINGHAL. "Computational simulation of concurrent engineering for aerospace propulsion systems." In Aerospace Design Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-1144.

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Czysz, Paul. "For hypersonic design propulsion sharpens the focus." In Aircraft Design, Systems, and Operations Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-4012.

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MELLO, J., and D. KOTANSKY. "Aero/propulsion technology for STOL and maneuver." In Aircraft Design Systems and Operations Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1985. http://dx.doi.org/10.2514/6.1985-4013.

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Reports on the topic "Propulsion systems design"

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Gulczinski, Frank S., Schilling III, Hall John H., Woodward Christopher D., and Jonathan R. Powersail High Power Propulsion System Design Study. Fort Belvoir, VA: Defense Technical Information Center, June 2001. http://dx.doi.org/10.21236/ada409913.

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