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Relevant bibliographies by topics / Space engine / Dissertations / Theses

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Dissertations / Theses on the topic 'Space engine'

Author: Grafiati

Published: 28 May 2022

Last updated: 30 July 2025

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1

Yang, Feng. "Architecture, Virtual Space And Impossible Space." Thesis, KTH, Arkitektur, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-281401.

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This project investigates how to design an architecture in a context of virtual space, and how to utilise the exclusive possibilities of the virtual context. The main case study about the virtual space and impossible space is based on video games. After analysing the mechanism of building such 'impossible spaces' in various video games, this project conducted an experiment on designing several virtual spaces in the game engine, Unreal Engine 4, to investigate the differences between architecture in the real space and in the virtual space. In addition, another architecture experiment was condu

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2

Werner, Steven P. "Initiator diffraction limits for pulse detonation engine operation." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2002. http://library.nps.navy.mil/uhtbin/hyperion-image/02Dec%5FWerner.pdf.

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Thesis (M.S. in Astronautical Engineering)--Naval Postgraduate School, December 2002.<br>Thesis advisor(s): Christopher M. Brophy, Jose O. Sinibaldi. Includes bibliographical references (p. 45-47). Also available online.

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3

Besson, Vincent. "Parameter space robust control for S.I. engine idle speed." Thesis, University of Liverpool, 1998. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.366369.

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4

Jensen, Jonathan Andrew. "Robust discrete estimation of the space shuttle main engine." Thesis, Massachusetts Institute of Technology, 1996. http://hdl.handle.net/1721.1/49608.

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5

Sastry, Sudeep. "A Thermoacoustic Engine Refrigerator System for Space Exploration Mission." Case Western Reserve University School of Graduate Studies / OhioLINK, 2011. http://rave.ohiolink.edu/etdc/view?acc_num=case1301588899.

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6

Romanov, Artyom. "Rocket Engine System Analysis : Vinci Engine Turbines Analysis, Volvo Aero Corp." Thesis, Linköping University, Linköping University, Linköping University, Applied Thermodynamics and Fluid Mechanics, 2008. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-17766.

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<p>Major part of the current work describes the development of the update methodology for onedimensional code (TML) currently used at Volvo Aero Corporation during turbine design process. The methodology is then applied and tried out in a general engine analysis (GESTPAN).</p>

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7

Youssef, Hazim S. "Laser engine simulation using pressure based navier-stokes solver." Diss., This resource online, 1994. http://scholar.lib.vt.edu/theses/available/etd-10052007-143624/.

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8

Ho, Nhut Tan 1974. "Failure detection and isolation for the Space Shuttle Main Engine." Thesis, Massachusetts Institute of Technology, 1998. http://hdl.handle.net/1721.1/9909.

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9

Masson, Philippe. "Exploring Space-Time Trade-Offs in the SAP NetWeaver Engine TREX." Zürich : [Institut für Informationssysteme, Eidgenössische Technische Hochschule Zürich], 2008. http://e-collection.ethbib.ethz.ch/show?type=dipl&nr=358.

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10

Al, Ruqeishi Khalil. "Self-adapting parallel metric-space search engine for variable query loads." Thesis, Aston University, 2016. http://publications.aston.ac.uk/28552/.

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This research focuses on automatically adapting a search engine size in response to fluctuations in query workload. Deploying a search engine in an Infrastructure as a Service (IaaS) cloud facilitates allocating or deallocating computer resources to or from the engine. Our solution is to contribute an adaptive search engine that will repeatedly re-evaluate its load and, when appropriate, switch over to a dierent number of active processors. We focus on three aspects and break them out into three sub-problems as follows: Continually determining the Number of Processors (CNP), New Grouping Probl

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11

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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12

Kayes, David J. (David Jonathan) 1972. "Crank angle and space resolved, speciated sampling of engine-out exhaust hydrocarbons." Thesis, Massachusetts Institute of Technology, 1996. http://hdl.handle.net/1721.1/40007.

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13

Brown, Joseph R. "Model Identification for the Space Shuttle Main Engine High Pressure Oxidizer Turbopump." Ohio University / OhioLINK, 1992. http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1239733713.

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14

Suchocki, James Alexander. "Operational Space and Characterization of a Rotating Detonation Engine Using Hydrogen and Air." The Ohio State University, 2012. http://rave.ohiolink.edu/etdc/view?acc_num=osu1330266587.

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15

Greco, Philip Andrew. "Turbine performance mapping of the space-shuttle main engine high-pressure fuel turbopump." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1995. http://handle.dtic.mil/100.2/ADA306473.

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Thesis (M.S. in Aeronautical Engineering) Naval Postgraduate School, September 1995.<br>Thesis advisor(s): Garth V. Hobson. "September 1995." Includes bibliographical references. Also available online.

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16

Southward, James D. "Laser doppler velocimetry in the space-shuttle main engine high-pressure fuel turbopump." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1998. http://handle.dtic.mil/100.2/ADA342224.

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Thesis (M.S. in Aeronautical Engineering) Naval Postgraduate School, March 1998.<br>Thesis advisor(s): Garth V. Hobson. "March 1998." Includes bibliographical references (p. 145-147). Also available online.

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17

Li, Yi-Hsien. "Real-Time Space-Time Adaptive Processing on the STI CELL Multiprocessor." Thesis, Linköping University, Department of Electrical Engineering, 2007. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-8933.

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<p>Space-Time Adaptive Processing (STAP) has been widely used in modern radar systems such as Ground Moving Target Indication (GMTI) systems in order to suppress jamming and interference. However, the high performance comes at a price of higher computational complexity, which requires extensive powerful hardware.</p><p>The new STI Cell Broadband Engine (CBE) processor combines PowerPC core augmented with eight streamlined high-performance SIMD processing engine offers an opportunity to implement the STAP baseband signal processing without any full custom hardware. This paper presents the imple

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18

Li, Qingyuan. "Development and refinement of a hybrid electric vehicle simulator and its application in "design space exploration" /." Connect to this title online, 1998. http://rave.ohiolink.edu/etdc/view?acc%5Fnum=osu11085884154.

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19

Yoshida, Brian Richard. "Compuational analysis of boundary layer control by suction in a space transfer vehicle engine turbopump diffuser /." Online version of thesis, 1992. http://hdl.handle.net/1850/11058.

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20

Tidefelt, Henrik. "Applied Output Error Identification: SI Engine Under Normal Operating Conditions." Thesis, Linköping University, Department of Electrical Engineering, 2004. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-2380.

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<p>This report presents work done in the field of output error identification, with application to spark ignition (SI) engine identification for the purpose of air to fuel ratio control. The generic parts of the project consist mainly in setting out the basis for the design of output error identification software. Efficiency issues related to linear state space models have also been explored, and although the software design is not made explicit in this report, many of the important concepts have been implemented in order to provide powerful abstractions for the application to SI engine identi

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21

Wissinger, Gordon J. "Computational analysis of space transfer vehicle engine turbopump diffuser design for deep-throttling : by Gordon J. Wissinger /." Online version of thesis, 1991. http://hdl.handle.net/1850/11001.

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22

Estublier, Denis L. "Radiation emission and absorption in a hydrogen plasma of a laser engine." Thesis, Virginia Tech, 1990. http://hdl.handle.net/10919/42161.

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<p>In this work, we describe all the possible radiative processes occuring in a low temperature hydrogen plasma. Some of the fundamental concepts involving ionized gases and collision phenomena are presented, and a rigourous approach is used to show that classical mechanics is quite appropriate to our study.</p> <p> As an application to a laser engine, we investigate the effects of the maximum temperature, the temperature gradient, the stretching of the plasma shape, the engine pressure, and the equivalent sphere radius, on the total emitted power, including absorbing mechanisms through the eq

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23

Ščeponavičius, Audrius. "Kosminio žingsninio strateginio žaidimo kūrimas. Game Engine projektavimas ir realizavimas." Bachelor's thesis, Lithuanian Academic Libraries Network (LABT), 2010. http://vddb.laba.lt/obj/LT-eLABa-0001:E.02~2010~D_20100907_094331-26453.

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Darbas skirtas sukurti pasaulio modelio modulio dalį, susijusią su resursų kūrimu. Darbo metu atlikta šios dalies poreikių analizė bei sukurtas realizacijos projektas. Remiantis šiuo projektu buvo sukurta pasaulio modulio dalis atsakinga už pasaulio modelio resursus, gebanti resursus klasifikuoti, bei atlikti resursų kūrimo, trynimo, panaudojimo veiksmus.<br>The purpose of work is to create part of world model module which is associated with resource creation. In the course of this work requirements for this part of module were analyzed and an implementation project was made. Using this projec

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Barauskas, Nerijus. "Kosminio žingsninio strateginio žaidimo kūrimas. Game engine projektavimas ir realizavimas." Bachelor's thesis, Lithuanian Academic Libraries Network (LABT), 2010. http://vddb.laba.lt/obj/LT-eLABa-0001:E.02~2010~D_20100907_094605-09824.

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Darbas skirtas sukurti žaidimo variklio pasaulio modelį palaikantį modulį. Darbo metu buvo atlikta žaidimo pasaulio modelio poreikių analizė ir suprojektuotas pasaulio modelį palaikantis modulis. Pagal šį projektą buvo sukurtas pasaulio modelį palaikantis įrankis bei jo efektyvumą kontroliuojantis pagalbinis įrankis. Sukurtas įrankis leidžia realizuoti ne vieną kosminio žingsninio strateginio žaidimo pasaulio modelį, turintį kiek įmanoma mažiau apribojimų.<br>The purpose of this work is to create a module that supports the world concept, for the game engine. In the course of this work requirem

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25

Niang, Samuel. "Optimisation of positron accumulation in the GBAR experiment and study of space propulsion based on antimatter." Thesis, université Paris-Saclay, 2020. http://www.theses.fr/2020UPASP075.

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Le but de l'expérience GBAR est de déterminer l'effet de la gravité sur des atomes d'anti-hydrogène. Les atomes d'anti-hydrogène sont créés en neutralisant des ions anti-hydrogène grâce à un faisceau laser. Un ion d'anti-hydrogène étant produit par la capture de deux positons par un antiproton volant dans un nuage de positronium. Pour cela, 10 x 10¹⁰ positons doivent être envoyés sur une cible de silicate nanoporeuse de laquelle va ressortir le nuage de positronium. Les positons sont produits par un LINAC (accélérateur linéaire), accélérant des électrons à 9 MeV sur une cible de tungsten. Ce p

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26

PAISSONI, CHRISTOPHER ANDREA. "Comprehensive approach to electric propulsion for innovative space platforms." Doctoral thesis, Politecnico di Torino, 2021. http://hdl.handle.net/11583/2945189.

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27

Hemmings, Stephen. "Supporting the regeneration process of a diesel particulate filter with the addition of hydrogen and hydrogen/carbon monoxide mixtures : diesel engine aftertreatment system." Thesis, Brunel University, 2012. http://bura.brunel.ac.uk/handle/2438/7073.

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This investigation aims to enhance the regeneration performance of a diesel particulate filter. This is achieved by introducing various chemical components to the regeneration process, which are representative of what can be generated ‘on board’ a vehicle using an exhaust gas fuel reformer. By researching the effects of introducing such components using a periodic injection cycle the aim is to reduce the volume of ‘reformates’ required to assist in proficient diesel particulate filter regeneration. As a result, this study also aims to support future work in the development of exhaust gas fuel

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28

Rutkowski, Richard J. "Cold flow simulation of the alternate turbopump development turbine of the space shuttle main engine high pressure fuel turbopump." Thesis, Monterey, California. Naval Postgraduate School, 1994. http://hdl.handle.net/10945/28034.

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Approved for public release; distribution is unlimited<br>Completion of the installation at the Naval Postgraduate School of a cold-flow test facility for the turbine of the Space Shuttle Main Engine High Pressure Fuel Turbopump is reported. The article to be tested is the first stage of the Alternate Turbopump Development model designed and manufactured by Pratt & Whitney. The purpose of the facility is to enable the development of non- intrusive flow measurements and comparison of those measurements with numerical simulations. Flow field characteristics of the turbine stator were predicted u

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29

McKee, Joseph R. "Experimental and computational investigation of cold-flow through the turbine of the space-shuttle main engine high-pressure fuel turbopump." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1998. http://handle.dtic.mil/100.2/ADA356000.

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Thesis (M.S. in Aeronautical Engineering) Naval Postgraduate School, September 1998.<br>"September 1998." Thesis advisor(s): Garth V. Hobson. Includes bibliographical references (p. 115-116). Also available online.

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30

Studevan, Colin C. "Design of a cold-flow test facility for the high-pressure fuel turbopump turbine of the space-shuttle main engine." Thesis, Monterey, California. Naval Postgraduate School, 1993. http://hdl.handle.net/10945/19733.

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Approved for public release; distribution is unlimited<br>The design and installation at the Naval Postgraduate School of a cold-flow test facility for the turbine of the high-pressure fuel turbopump of the Space Shuttle Main Engine, is reported. The specific article to be tested is the 'Alternate Development Model' designed and manufactured by Pratt & Whitney. The design of individual components is documented. The installation of the facility subsystem is described in detail. A preliminary estimation of turbine performance is made.

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31

Gordon, Kayleigh Elizabeth. "Analysis of Chinese Cryogenic Long March Launch Vehicles and YF-100 Liquid Rocket Engine." The Ohio State University, 2018. http://rave.ohiolink.edu/etdc/view?acc_num=osu1524154852226897.

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32

Záleta, Martin. "Srovnání volně dostupných zobrazovacích knihoven." Master's thesis, Vysoké učení technické v Brně. Fakulta informačních technologií, 2013. http://www.nusl.cz/ntk/nusl-236408.

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The main purpose of this paper is to provide a detailed analysis of some of the major available open source rendering libraries with the emphasis on their notable characteristics, and an in-depth comparison among them with regards to their possible practical use. Specifically, the selected rendering libraries in this paper are the following - OpenSceneGraph, Ogre 3D, Irrlicht Engine, Crystal Space and OpenSG, but a sidenote is given to some of the others as well. Last but not least, self-made examples of their usage are also included, and are meant to demonstrate some of the mentioned characte

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Черненко, В. В., та М. А. Погорєлий. "Різновиди космічних двигунів". Thesis, Сумський державний університет, 2018. http://essuir.sumdu.edu.ua/handle/123456789/67086.

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34

Bulut, Jane. "Design and CFD analysis of the demonstrator aerospike engine for a small satellite launcher application." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2020.

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Starting with a brief overview of thrust generation for launchers, this study focuses on the design process of the demonstrator aerospike engine, DEMOP-1, of the Pangea Aerospace's commercial grade engine and its flow field analysis. The primary goal of the study is to obtain the plug nozzle design delivers 30 kN thrust using cryogenic liquid oxygen (LOX) as the oxidizer and cryogenic liquid methane (LCH4) as the fuel, with the mixture ratio of 3.4. Design parameters considered as 30 bar of combustion chamber pressure (Po) and expansion ratio as 15 for an optimum expanded nozzle. On the basi

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35

Pecino, Rodriguez Jose Ignacio. "Portfolio of original compositions : dynamic audio composition via space and motion in virtual and augmented environments." Thesis, University of Manchester, 2015. https://www.research.manchester.ac.uk/portal/en/theses/portfolio-of-original-compositions-dynamic-audio-composition-via-space-and-motion-in-virtual-and-augmented-environments(637e9f5b-7d42-4214-92c4-70bac912cec2).html.

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Electroacoustic music is often regarded as not being sufficiently accessible to the general public because of its sound-based abstract quality and the complexity of its language. Live electronic music introduces the figure of the performer as a gestural bodily agent that re-enables our multimodal perception of sound and seems to alleviate the accessibility dilemma. However, live electronic music generally lacks the level of detail found in studio-based fixed media works, and it can hardly be transferred outside the concert hall situation (e.g. as a video recording) without losing most of its f

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36

Wahlström, Dennis. "Probabilistic Multidisciplinary Design Optimization on a high-pressure sandwich wall in a rocket engine application." Thesis, Umeå universitet, Institutionen för fysik, 2017. http://urn.kb.se/resolve?urn=urn:nbn:se:umu:diva-138480.

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A need to find better achievement has always been required in the space industrythrough time. Advanced technologies are provided to accomplish goals for humanityfor space explorer and space missions, to apprehend answers and widen knowledges. These are the goals of improvement, and in this thesis, is to strive and demandto understand and improve the mass of a space nozzle, utilized in an upperstage of space mission, with an expander cycle engine. The study is carried out by creating design of experiment using Latin HypercubeSampling (LHS) with a consideration to number of design and simulation

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37

Ekström, Marcus. "Communication tool in virtual reality – A telepresence alternative : An alternative to telepresence – bringing the shared space to a virtual environment in virtual reality." Thesis, Mittuniversitetet, Avdelningen för informationssystem och -teknologi, 2017. http://urn.kb.se/resolve?urn=urn:nbn:se:miun:diva-31450.

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Videoconferencing is one of the most common telepresence methods today and educational videos is rising in popularity among distance learners. Traditional videoconferencing is unable to convey gestures and mutual eye contact between participants. This study aim to propose a Virtual Reality telepresence solution using game engines. A literature study confirmed the effectiveness achieved in VR is comparable to the effectiveness in face-to-face meetings. The suggested solution implements whiteboard functionality from a real-life perspective, confirming it is possible to include new functionality

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38

Bernardi, Jean de. "Aspects expérimentaux et théoriques des instabilités de cavitation dans les turbopompes de moteurs de fusée." Grenoble INPG, 1996. http://www.theses.fr/1996INPG0217.

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Les instabilités hydrauliques et les efforts radiaux générés par la cavitation partielle sur un inducteur de turbopompe ont été étudiés en eau pour les inducteurs des turbopompes à hydrogène et à oxygène du moteur VULCAIN d’ARIANE 5. Nous avons pu établir une méthode d’identification et d’analyse des instabilités à l’aide de la synchronisation de films rapides avec des mesures d’effort, sur l’axe et avec des signaux de pression instationnaire en paroi. Des fréquences caractéristiques du phénomène de cavitation instationnaire ont alors été identifiées à différents points de fonctionnement. Cett

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Messineo, Jérôme. "Modélisation des instabilités hydrodynamiques dans les moteurs-fusées hybrides." Thesis, Toulouse, ISAE, 2016. http://www.theses.fr/2016ESAE0025/document.

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Les moteurs-fusées hybrides combinent les technologies des deux autres catégories de moteurs à propulsionchimique, et associent un combustible et un oxydant stockés respectivement sous phase solide et liquide.Cette architecture offre un certain nombre d’avantages, comme par exemple des coûts plus faibleset une architecture simplifiée par rapport à la propulsion bi-liquide; la possibilité de réaliser de multiplesextinctions et ré-allumages et une bonne impulsion spécifique théorique par rapport à la propulsion solide,et enfin une sécurité de mise en œuvre accrue et un impact environnemental fai

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Sakai, Tadashi. "A Study of Variable Thrust, Variable Specific Impulse Trajectories for Solar System Exploration." Diss., Georgia Institute of Technology, 2004. http://hdl.handle.net/1853/4904.

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A study has been performed to determine the advantages and disadvantages of variable thrust and variable specific impulse (Isp) trajectories for solar system exploration. There have been several numerical research efforts for variable thrust, variable Isp, power-limited trajectory optimization problems. All of these results conclude that variable thrust, variable Isp (variable specific impulse, or VSI) engines are superior to constant thrust, constant Isp (constant specific impulse, or CSI) engines. However, most of these research efforts assume a mission from Earth to Mars, and some of them

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Kratz, Jonathan L. "Robust Control of Uncertain Input-Delayed Sample Data Systems through Optimization of a Robustness Bound." The Ohio State University, 2015. http://rave.ohiolink.edu/etdc/view?acc_num=osu1429149093.

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Girardello, Carlo. "Optical Analysis of Plasma : Flame Emission in Cryogenic Rocket Engines." Thesis, Luleå tekniska universitet, Rymdteknik, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-76097.

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This thesis contains the results of optical flame emission measurements of the Vulcain 2.1engine and the plasma emission spectroscopy of the Lumen Project engine. The plume spectroscopyis analyzed, ordered and studied in detail to offer the best possible molecular composition.The main focus relied on the hydroxide radical, blue radiation and other moleculesanalysis of the intensities encountered during the tests. The plasma emission spectroscopy isfocused on the determination of the plasma temperature value in LIBS measurements. Thehydrogen plasma temperature determination of the local thermod

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43

Gidugu, Praveen. "Effect of adding a regenerator to Kornhauser's MIT "two-space" test rig." Cleveland, Ohio : Cleveland State University, 2008. http://rave.ohiolink.edu/etdc/view?acc_num=csu1212595450.

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Thesis (M.S.)--Cleveland State University, 2008.<br>Abstract. Title from PDF t.p. (viewed on July 9, 2008). Includes bibliographical references (p. 100-103). Available online via the OhioLINK ETD Center. Also available in print.

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Fors, Erik. "Time and Space Resolved Measurements from Rocket Engines." Thesis, KTH, Rymd- och plasmafysik, 2012. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-104042.

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Equipment planned to be part of space missions is put through a substantial series of tests inorder to ensure a very high degree of reliability. This also applies to the HPGP thrusters manufactured by ECAPS AB. While conducting live fire tests the temperature is monitored using two separate systems, one pyrometer and one Infrared camera. The two systems show a difference in temperature for the same spot on the thruster. This is believed to be due to changes in the emissivity. An experimental setup is designed in order to measure the behavior of the emissivity of this material to decrease measu

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Consigny, Pierre. "Time and Space Resolved Measurements from Rocket Engines." Thesis, KTH, Kraft- och värmeteknologi, 2012. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-120479.

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46

Silvestrini, Jorge Hugo. "Simulation des grandes échelles des zones de mélange : application à la propulsion solide des lanceurs spatiaux." Grenoble INPG, 1996. http://www.theses.fr/1996INPG0104.

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On presente le formalisme de la simulation des grandes echelles (les) pour l'etude des ecoulements turbulents incompressibles et compressibles, puis les modeles sous-maille qui tiennent compte des echelles plus petites que la maille de calcul. Des tests, en configuration de couche de melange temporelle, permettent de mettre en evidence le comportement de differents modeles. Ensuite, des les des couches de melanges tridimensionnelles temporelles et spatiales sont presentees. Dans le deux cas, on teste deux types de perturbations sur la condition initiale (condition d'entree pour le probleme spa

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Alluri, Chandra M. "Testing calculation engines using input space partitioning and automation." Fairfax, VA : George Mason University, 2008. http://hdl.handle.net/1920/3228.

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Thesis (M.S.)--George Mason University, 2008.<br>Vita: p. 158. Thesis director: Jeff Offutt. Submitted in partial fulfillment of the requirements for the degree of Master of Science in Software Engineering. Title from PDF t.p. (viewed Aug. 27, 2008). Includes bibliographical references (p. 156-157). Also issued in print.

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Mukherjee, Smarajit. "Time- and Space-resolved Heat Transfer Model for Spark-Ignition Engines." The Ohio State University, 2018. http://rave.ohiolink.edu/etdc/view?acc_num=osu1517440404339384.

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Rocchi, Jean-Philippe. "Simulations aux grandes échelles de la phase d'allumage dans un moteur fusée cryotechnique." Phd thesis, Toulouse, INPT, 2014. http://oatao.univ-toulouse.fr/14667/1/rocchi.pdf.

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À ses débuts, la conquête spatiale a pu bénéficier des rivalités politiques de la Guerre Froide pour se développer rapidement sans réellement se soucier des efforts économiques à fournir. Aujourd’hui, de nombreux pays subissent le revers de la médaille de cette course effrénée : pour maintenir une flotte de lanceurs viable économiquement, les différentes agences spatiales doivent faire face à un dilemme opposant la minimisation des coûts de lancement à la maximisation de leur fiabilité. Dans cette logique d’optimisation, les industriels présents dans ce processus de réflexion se tournent vers

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Josselyn, Scott B. "Optimization of low thrust trajectories with terminal aerocapture." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2003. http://library.nps.navy.mil/uhtbin/hyperion-image/03Jun%5FJosselyn.pdf.

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Thesis (Aeronautical and Astronautical Engineer)--Naval Postgraduate School, June 2003.<br>Thesis advisor(s): I. Michael Ross, Steve Matousek. Includes bibliographical references (p. 149-150). Also available online.

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