.bib file sample (BSc thesis)

2015-bsc-project-leto.bib

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@misc{fig-bi-elliptical,
author = {Buck, Andrew},
title = {{File:Bi-elliptic transfer.svg - Wikimedia Commons}},
url = {http://commons.wikimedia.org/wiki/File:Bi-elliptic{\_}transfer.svg},
urldate = {2015-06-06}
}
@misc{Roussel2005,
author = {Roussel, Marc R},
file = {:Users/gandalf/Library/Mobile Documents/com{\~{}}apple{\~{}}CloudDocs/-Sync/Mendeley/Roussel/Roussel - 2005 - Hamiltonian systems.pdf:pdf},
pages = {1--9},
title = {{Hamiltonian systems}},
year = {2005}
}
@misc{stack-euler-lagrange,
author = {Stackexchange},
title = {{Stackexchange Mathematics - Who came up with the Euler-Lagrange equation first?}},
url = {http://math.stackexchange.com/questions/177243/who-came-up-with-the-euler-lagrange-equation-first},
urldate = {2015-06-02}
}
@book{Goldstine1980,
author = {Goldstine, Herman Heine},
edition = {First Edit},
isbn = {3540905219},
pages = {410},
publisher = {Springer-Verlag},
title = {{A history of the calculus of variations from the 17th through the 19th century}},
url = {https://books.google.com/books?id=ymQPAQAAMAAJ{\&}pgis=1},
year = {1980}
}
@misc{apollo-orbit-altitude,
author = {NASA},
title = {{Apollo 11 Lunar Orbit Phase}},
url = {http://history.nasa.gov/SP-4029/Apollo{\_}11g{\_}Lunar{\_}Orbit{\_}Phase.htm},
urldate = {2015-06-05}
}
@misc{wiki-spacex,
author = {Wikipedia},
title = {{Wikipedia - SpaceX}},
urldate = {2015-06-04}
}
@misc{Peet,
author = {Peet, Matthew M.},
file = {:Users/gandalf/Library/Mobile Documents/com{\~{}}apple{\~{}}CloudDocs/-Sync/Mendeley/Peet/Peet - Unknown - Spacecraft and Aircraft Dynamics - Lecture 9 Bi-elliptics and Out-of-Plane Maneuvers.pdf:pdf},
keywords = {Course presentation slides},
mendeley-tags = {Course presentation slides},
publisher = {Illinois Institute of Technology},
title = {{Spacecraft and Aircraft Dynamics - Lecture 9: Bi-elliptics and Out-of-Plane Maneuvers}},
url = {http://mmae.iit.edu/{~}mpeet/Classes/MMAE441/Spacecraft/441Lecture21.pdf}
}
@misc{nasa-apollo-launch-window,
author = {NASA},
title = {{Launch Windows Essay}},
url = {http://history.nasa.gov/afj/launchwindow/lw1.html},
urldate = {2015-06-08}
}
@misc{wiki-llo,
author = {Wikipedia},
title = {{Wikipedia - Lunar orbit}},
url = {http://en.wikipedia.org/wiki/Lunar{\_}orbit},
urldate = {2015-06-11}
}
@article{Garcia2007,
abstract = {This paper is devoted to clarify the algorithmic definition of the weak stability boundary in the framework of the planar Restricted Three Body Problem. The role of the invariant hyperbolic manifolds associated to the central manifolds of the libration points L1 and L2, as boundary of the weak stability region, is shown.},
author = {Garc{\'{i}}a, F. and G{\'{o}}mez, G.},
doi = {10.1007/s10569-006-9053-6},
file = {:Users/gandalf/Library/Mobile Documents/com{\~{}}apple{\~{}}CloudDocs/-Sync/Mendeley/Garc{\'{i}}a, G{\'{o}}mez/Garc{\'{i}}a, G{\'{o}}mez - 2007 - A note on weak stability boundaries.pdf:pdf},
isbn = {1056900690536},
issn = {09232958},
journal = {Celestial Mechanics and Dynamical Astronomy},
keywords = {Invariant manifolds,Libration points,Weak stability boundaries},
number = {2},
pages = {87--100},
title = {{A note on weak stability boundaries}},
volume = {97},
year = {2007}
}
@techreport{Juul2008,
author = {Juul, Jeppe S{\o}gaard},
file = {:Users/gandalf/Library/Mobile Documents/com{\~{}}apple{\~{}}CloudDocs/-Sync/Mendeley/Juul/Juul - 2008 - Low Energy Trajectories to the Moon.pdf:pdf},
institution = {University of Copehagen},
pages = {36},
title = {{Low Energy Trajectories to the Moon}},
url = {http://jeppejuul.com/research/projects/bachelors-project-low-energy-trajectories-to-the-moon/},
year = {2008}
}
@inproceedings{Belbruno2000,
address = {Denver, Colerado},
author = {Belbruno, Edward a and Carrico, John P},
booktitle = {Astrodynamics specialist conference},
doi = {doi:10.2514/6.2000-4142},
file = {:Users/gandalf/Library/Mobile Documents/com{\~{}}apple{\~{}}CloudDocs/-Sync/Mendeley/Belbruno, Carrico/Belbruno, Carrico - 2000 - Calculation of Weak Stability Boundary Ballistic Lunar Transfer Trajectories.pdf:pdf},
title = {{Calculation of Weak Stability Boundary Ballistic Lunar Transfer Trajectories}},
year = {2000}
}
@book{Murray1999,
author = {Murray, Carl D. and Dermott, Stanley F.},
edition = {1st},
isbn = {0-521-57295-9},
pages = {592},
publisher = {Cambridge University Press},
title = {{Solar System Dynamics}},
year = {1999}
}
@article{Biesbroek2000,
author = {Biesbroek, R and Janin, G},
file = {:Users/gandalf/Library/Mobile Documents/com{\~{}}apple{\~{}}CloudDocs/-Sync/Mendeley/Biesbroek, Janin/Biesbroek, Janin - 2000 - Ways to the Moon.pdf:pdf},
journal = {Earth},
number = {august},
pages = {92--99},
title = {{Ways to the Moon?}},
year = {2000}
}
@misc{laursen,
author = {Laursen},
keywords = {LaTeX template},
title = {{{\_}laursen / Laursen's XeLaTeX thesis template — Bitbucket}},
url = {https://bitbucket.org/{\_}laursen/laursens-xelatex-thesis-template/overview},
urldate = {2015-05-29}
}
@inproceedings{Belbruno2007,
author = {Belbruno, Edward},
booktitle = {NASA Science Technology Conference 2007},
file = {:Users/gandalf/Library/Mobile Documents/com{\~{}}apple{\~{}}CloudDocs/-Sync/Mendeley/Belbruno/Belbruno - 2007 - Low Energy Motions in the Earth-Moon System, Chaos, and Weak Capture.pdf:pdf},
title = {{Low Energy Motions in the Earth-Moon System, Chaos, and Weak Capture}},
url = {http://esto.nasa.gov/conferences/nstc2007/papers/Belbruno{\_}Edward{\_}C6P1{\_}NSTC-07-0156.pdf},
year = {2007}
}
@misc{RossAndersen,
author = {Andersen, Ross},
title = {{The Elon Musk interview on Mars colonisation – Ross Andersen – Aeon}},
url = {http://aeon.co/magazine/technology/the-elon-musk-interview-on-mars/},
urldate = {2015-06-04}
}
@misc{ucsd-quadratic,
author = {Branson, Jim},
title = {{Recalling Lagrangian Mechanics}},
url = {http://hepweb.ucsd.edu/ph110b/110b{\_}notes/node86.html},
urldate = {2015-06-08},
year = {2012}
}
@book{Goldstein2002,
abstract = {For thirty years this has been the acknowledged standard in advanced classical mechanics courses. This text enables students to make connections between classical and modern physics. In this edition, Beams Medal winner Charles Poole and John Safko have updated the text to include the latest topics, applications, and notation, to reflect today's physics curriculum. They introduce students to the increasingly important role that nonlinearities play in contemporary applications of classical mechanics. Numerical exercises help students to develop skills in how to use computer techniques to solve problems in physics. Mathematical techniques are presented in detail so that the text remains fully accessible to students who have not had an intermediate course in classical mechanics.},
author = {Goldstein, Herbert and Poole, Charles P. and Safko, John L.},
edition = {3rd},
isbn = {0201657023},
pages = {638},
publisher = {Addison Wesley},
title = {{Classical Mechanics}},
url = {https://books.google.dk/books/about/Classical{\_}Mechanics.html?id=tJCuQgAACAAJ{\&}pgis=1},
year = {2002}
}
@misc{wiki-lag,
author = {Wikipedia},
title = {{Wikipedia: Lagrangian - Advantages over other methods}},
url = {http://en.wikipedia.org/wiki/Lagrangian{\#}Advantages{\_}over{\_}other{\_}methods},
urldate = {2015-06-01}
}
@article{Prussing1992,
author = {Prussing, John E.},
doi = {10.2514/3.20941},
issn = {0731-5090},
journal = {Journal of Guidance, Control, and Dynamics},
language = {en},
month = {jul},
number = {4},
pages = {1037--1038},
title = {{Simple proof of the global optimality of the Hohmann transfer}},
url = {http://arc.aiaa.org.globalproxy.cvt.dk/doi/abs/10.2514/3.20941},
volume = {15},
year = {1992}
}
@misc{bcc-obama-moon,
author = {BBC},
keywords = {BBC,BBC News,News,british,foreign,international,news online,online,service,uk,world},
title = {{BBC News - Obama cancels Moon return project}},
url = {http://news.bbc.co.uk/2/hi/science/nature/8489097.stm},
urldate = {2015-06-04}
}
@misc{esa-soyuz,
author = {ESA},
keywords = {Docking And Berthing Of Spacecraft,European Space Agency (Space Agency),International Space Station (Satellite),Soyuz (Spacecraft),Space Rendezvous,jour...},
title = {{Soyuz rendezvous and docking explained}},
url = {https://www.youtube.com/watch?v=M2{\_}NeFbFcSw{\&}feature=youtu.be{\&}t=9m55s},
year = {2014}
}
@book{Lanczos1970,
author = {Lanczos, Cornelius},
edition = {Fourth Edi},
isbn = {978-0486650678},
pages = {418},
publisher = {Dover Publications},
title = {{The Variational Principles of Mechanics}},
year = {1970}
}
@misc{fauske,
author = {Fauske, Kjell Magne},
title = {{Global nodes | TikZ example}},
url = {http://www.texample.net/tikz/examples/global-nodes/},
urldate = {2015-05-29}
}
@article{Topputo2014,
archivePrefix = {arXiv},
arxivId = {1410.8856},
author = {Topputo, Francesco and Belbruno, E},
doi = {10.1007/s10569-015-9605-8},
eprint = {1410.8856},
file = {:Users/gandalf/Library/Mobile Documents/com{\~{}}apple{\~{}}CloudDocs/-Sync/Mendeley/Topputo, Belbruno/Topputo, Belbruno - 2014 - Earth--Mars Transfers with Ballistic Capture.pdf:pdf},
issn = {0923-2958},
journal = {arXiv preprint arXiv:1410.8856},
pages = {1--21},
title = {{Earth--Mars Transfers with Ballistic Capture}},
url = {http://arxiv.org/abs/1410.8856},
year = {2014}
}
@misc{apollo-parking,
author = {Wheeler, Robin},
title = {{Apollo lunar landing launch window: The controlling factors and constraints}},
url = {http://history.nasa.gov/afj/launchwindow/lw1.html{\#}EPO},
urldate = {2015-06-04}
}
@inproceedings{Topputo2005,
abstract = {In the frame of the lunar exploration, numerous future space missions will require maximization of payload mass, and simultaneously achieving reasonable transfer times. To fulfill this request, low energy non-Keplerian orbits could be used to reach the Moon instead of high energetic transfers. The low energy solutions can be separated into two main categories depending on the nature of the trajectory approaching the Moon: low energy transit orbits that approach the Moon from the interior equilibrium point L(1) and weak stability boundary transfers that reach the Moon after passing through L(2). This paper proposes an alternative way to exploit the opportunities offered by L(1) transit orbits for the design of Earth-Moon transfers. First, in a neighborhood of the L(1) point, the three-body dynamics is linearized and written in normal form; then the entire family of nonlinear transit orbits is obtained by selecting the appropriate nontrivial amplitudes associated with the hyperbolic part. The L(1)-Earth arc is close to a 5:2 resonant orbit with the Moon, whose perturbations cause the apogee to rise. In a second step, two selected low altitude parking orbits around the Earth and the Moon are linked with the transit orbit by means of two three-body Lambert arcs, solutions of two two-point boundary value problems. The resulting Earth-to-Moon trajectories prove to be very efficient in the Moon captured arc and save approximately 100 m/sec in Deltav cost when compared to the Hohmann transfer. Furthermore, such solutions demonstrate that Moon capture could be obtained in the frame of the Earth-Moon R3BP neglecting the presence of the Sun.},
author = {Topputo, Francesco and Vasile, Massimiliano and Bernelli-Zazzera, Franco},
booktitle = {Annals of the New York Academy of Sciences},
doi = {10.1196/annals.1370.025},
file = {:Users/gandalf/Library/Mobile Documents/com{\~{}}apple{\~{}}CloudDocs/-Sync/Mendeley/Topputo, Vasile, Bernelli-Zazzera/Topputo, Vasile, Bernelli-Zazzera - 2005 - Earth-to-moon low energy transfers targeting L1 hyperbolic transit orbits.pdf:pdf},
issn = {00778923},
keywords = {Earth-moon low energy transfer,Hyperbolic Transit orbit,Libration point},
number = {June},
pmid = {16510403},
title = {{Earth-to-moon low energy transfers targeting L1 hyperbolic transit orbits}},
url = {https://www.researchgate.net/profile/Francesco{\_}Topputo/publication/45417269{\_}Earth-to-Moon{\_}Low{\_}Energy{\_}Transfers{\_}Targeting{\_}L1{\_}Hyperbolic{\_}Transit{\_}Orbits/links/0046351f230274d70a000000.pdf},
year = {2005}
}
@misc{noethers,
abstract = {An extremely powerful theorem in physics which states that each symmetry of a system leads to a physically conserved quantity. Symmetry under translation corresponds to conservation of momentum, symmetry under rotation to conservation of angular momentum, symmetry in time to conservation of energy, etc.},
author = {Weisstein, Eric W.},
keywords = {51M,Mathematics:Geometry:Transformations:Miscellaneous},
language = {en},
publisher = {Wolfram Research, Inc.},
title = {{Noether's Symmetry Theorem}},
url = {http://mathworld.wolfram.com/NoethersSymmetryTheorem.html}
}
@misc{ma,
address = {Champaign, Illinois},
author = {{Wolfram Research}, Inc.},
publisher = {Wolfram Research, Inc.},
title = {{Mathematica (see appendix "Mathematica Data" for details)}}
}
@misc{fig-hohmann,
author = {Bartkowiak, Hubert},
title = {{File:Hohmann transfer orbit.svg - Wikimedia Commons}},
url = {http://commons.wikimedia.org/wiki/File:Hohmann{\_}transfer{\_}orbit.svg},
urldate = {2015-06-06}
}
@misc{aerobraking,
author = {NASA},
keywords = {Earth,Europa,Grail,JPL,Jet Propulsion Laboratory,Jupiter,Lunar Portal,Mars,Mercury,Moon,NASA,National Aeronautics and Space Administration,Neptune,Planet,Planets,Pluto,SSE,Saturn,Solar System,Solar System Exploration,Space,Sun,Uranus,Venus,solarsystem},
title = {{NASA Solar System Exploration: Missions: By Name: MUSES-A}},
url = {http://solarsystem.nasa.gov/missions/profile.cfm?Sort=Alpha{\&}Alias=MUSES-A{\&}Letter=M{\&}Display=ReadMore},
urldate = {2015-06-04}
}
@book{Curtis2014,
abstract = {Up to now, we have mostly referenced the motion of orbiting objects to a nonrotating coordinate system fixed to the center of attraction (e.g., the center of the earth). This platform served as an inertial frame of reference, in which Newton's second law can be written as Fnet=maabsolute.},
author = {Curtis, Howard D.},
booktitle = {Orbital Mechanics for Engineering Students},
doi = {10.1016/B978-0-08-097747-8.00007-4},
edition = {3rd Editio},
file = {:Users/gandalf/Library/Mobile Documents/com{\~{}}apple{\~{}}CloudDocs/-Sync/Mendeley/Curtis/Curtis - 2014 - Orbital Mechanics for Engineering Students.pdf:pdf},
isbn = {9780080977478},
keywords = {Angular acceleration of comoving frame,Angular velocity of comoving frame,Clohessy–Wiltshire equations,Clohessy–Wiltshire matrices,LVLH frame,Orbital Mechanics,Relative acceleration in the comoving frame,Relative acceleration in the inertial frame,Textbook,Two-impulse rendezvous,r-bar},
mendeley-tags = {Orbital Mechanics,Textbook},
pages = {751},
pmid = {1272188},
publisher = {Elsevier},
title = {{Orbital Mechanics for Engineering Students}},
url = {http://www.sciencedirect.com/science/article/pii/B9780080977478000074},
year = {2014}
}
@book{Seefelder2002,
author = {Seefelder, Wolfgang},
edition = {1st},
isbn = {3-8316-0155-0},
pages = {171},
publisher = {Herbert Utz Verlag},
title = {{Lunar Transfer Orbits utilizing Solar Pertubations and Ballistic Capture}},
year = {2002}
}
@misc{cnn-bush-moon,
author = {CNN},
title = {{CNN.com - Bush unveils vision for moon and beyond - Jan. 15, 2004}},
url = {http://edition.cnn.com/2004/TECH/space/01/14/bush.space/},
urldate = {2015-06-04}
}
@misc{apollo-timeline,
author = {NASA},
title = {{Apollo 11 Mission Overview}},
url = {http://www.lpi.usra.edu/lunar/missions/apollo/apollo{\_}11/overview/},
urldate = {2015-06-11}
}
@misc{leo-cost,
author = {Coopersmith, Jonathan},
title = {{Affordable Access to Space | Issues in Science and Technology}},
url = {http://issues.org/29-1/jonathan/},
urldate = {2015-06-04}
}
@misc{wiki-quadratic,
author = {Wikipedia},
title = {{Wikipedia: Quadratic form}},
url = {http://en.wikipedia.org/wiki/Quadratic{\_}form},
urldate = {2015-06-02}
}
@article{Fraser1983,
author = {Fraser, Craig},
doi = {10.1007/BF00328268},
file = {:Users/gandalf/Library/Mobile Documents/com{\~{}}apple{\~{}}CloudDocs/-Sync/Mendeley/Fraser/Fraser - 1983 - J. L. Lagrange's early contributions to the principles and methods of mechanics.pdf:pdf},
issn = {00039519},
journal = {Archive for History of Exact Sciences},
number = {3},
pages = {197--241},
title = {{J. L. Lagrange's early contributions to the principles and methods of mechanics}},
url = {http://link.springer.com/10.1007/BF00328268},
volume = {28},
year = {1983}
}
@misc{fig-lagrange-points,
author = {Xander89},
title = {{File:Lagrange points2.svg - Wikimedia Commons}},
url = {https://commons.wikimedia.org/wiki/File:Lagrange{\_}points2.svg},
urldate = {2015-06-07}
}
@misc{nasa-llo,
author = {NASA},
title = {{Bizarre Lunar Orbits - NASA Science}},
url = {http://science.nasa.gov/science-news/science-at-nasa/2006/06nov{\_}loworbit/},
urldate = {2015-06-07}
}
@article{Marsden2006,
abstract = {... This paper will give a survey of some of these exciting ideas, and we would especially like to acknowledge the work of Michael Dellnitz , Frederic Gabern, Katalin Grubits, Oliver Junge, Wang-Sang Koon, Fran{\c{c}}ois Lekien, Martin Lo, Sina Ober-Bl{\"{o}}baum, Kathrin Padberg, Robert ...},
author = {Marsden, Jerrold E. and Ross, Shane D.},
file = {:Users/gandalf/Library/Mobile Documents/com{\~{}}apple{\~{}}CloudDocs/-Sync/Mendeley/Marsden, Ross/Marsden, Ross - 2006 - New methods in celestial mechanics and mission design.pdf:pdf},
issn = {0273-0979},
journal = {Bulletin of the American Mathematical Society},
number = {1},
pages = {43--73},
title = {{New methods in celestial mechanics and mission design}},
volume = {43},
year = {2006}
}
@inproceedings{NASA1966,
author = {NASA},
file = {:Users/gandalf/Library/Mobile Documents/com{\~{}}apple{\~{}}CloudDocs/-Sync/Mendeley/NASA/NASA - 1966 - Apollo Lunar Landing Mission Symposium.pdf:pdf},
title = {{Apollo Lunar Landing Mission Symposium}},
url = {http://www.hq.nasa.gov/alsj/LunarLandingMIssionSymposium1966{\_}1978075303.pdf},
year = {1966}
}
@article{Hochbruck2008,
author = {Hochbruck, Marlis},
file = {:Users/gandalf/Library/Mobile Documents/com{\~{}}apple{\~{}}CloudDocs/-Sync/Mendeley/Hochbruck/Hochbruck - 2008 - Symplectic Integrators.pdf:pdf},
title = {{Symplectic Integrators}},
url = {https://na.math.kit.edu/marlis/download/meetings/08Oberwolfach/symplectic1-print.pdf},
year = {2008}
}
@misc{astrobotic,
author = {Astrobotic},
title = {{Lunar Delivery | Astrobotic}},
url = {https://www.astrobotic.com/lunar-delivery},
urldate = {2015-06-04}
}
@article{Nakane2002,
author = {Nakane, Michiyo and Fraser, Craig G.},
doi = {10.1111/j.1600-0498.2002.tb00613.x},
file = {:Users/gandalf/Library/Mobile Documents/com{\~{}}apple{\~{}}CloudDocs/-Sync/Mendeley/Nakane, Fraser/Nakane, Fraser - 2002 - The Early History of Hamilton-Jacobi Dynamics 18341837.pdf:pdf},
issn = {0008-8994},
journal = {Centaurus},
month = {dec},
number = {3-4},
pages = {161--227},
title = {{The Early History of Hamilton-Jacobi Dynamics 1834?1837}},
url = {http://doi.wiley.com/10.1111/j.1600-0498.2002.tb00613.x},
volume = {44},
year = {2002}
}
@article{Sweetser1991,
abstract = {An estimate is found for a lower bound on the $\Delta$V needed for any trajectory which starts at 167 km altitude circular Earth orbit and ends in a 100 km altitude circular polar Lunar orbit. The analysis used involves calculations of Jacobi's intergral in a circular restricted three-body problem which approximates the Earth-Moon transfer problem. The result is an estimate that any such trajectory will require $\Delta$Vs of at least 3.099 km/s to leave the neighborhood of Earth and at least 0.622 km/s to achieve the desired orbit around the Moon, for a total of 3.721 km/s. Whether a trajectory exists which actually uses this $\Delta$V is not presently known, although recently Belbruno and Miller found an actual Earth-Moon trajectory which takes advantage of solar perturbations to achieve a transfer which has an injection $\Delta$V from Earth orbit of 3.187 km/s and an insertion $\Delta$V into Lunar orbit of 0.651 km/s.},
author = {Sweetser, Theodore H.},
isbn = {9780877033394},
issn = {00653438},
journal = {Advances in the Astronautical Sciences},
number = {pt 1},
pages = {111 -- 120},
title = {{Estimate of the global minimum DV needed for earth-moon transfer}},
volume = {75},
year = {1991}
}
@article{Koon2001,
annote = {F{\o}rste artikel udleveret af P. Hjorth.},
author = {Koon, W.S. and Lo, M. W. and Marsden, J. E. and Ross, S. D.},
file = {::},
journal = {Celestial Mechanics and Dynamical Astronomy},
number = {1-2},
pages = {63--73},
title = {{Low Energy Transfer to the Moon}},
url = {http://citeseerx.ist.psu.edu/viewdoc/summary?doi=10.1.1.307.2362},
volume = {81},
year = {2001}
}
@misc{unige-quadradic,
author = {Hairer, Ernst and Tu, M},
file = {:Users/gandalf/Library/Mobile Documents/com{\~{}}apple{\~{}}CloudDocs/-Sync/Mendeley/Hairer, Tu/Hairer, Tu - 2010 - Lecture 1 Hamiltonian systems.pdf:pdf},
keywords = {Course notes},
mendeley-tags = {Course notes},
title = {{Lecture 1 : Hamiltonian systems}},
url = {http://www.unige.ch/{~}hairer/poly{\_}geoint/week1.pdf},
urldate = {2015-06-08},
year = {2010}
}
@misc{wiki-low-earth-orbit,
author = {Wikipedia},
title = {{Wikipedia - Low-earth orbit}},
url = {http://en.wikipedia.org/wiki/Low{\_}Earth{\_}orbit},
urldate = {2015-06-04}
}
@misc{wiki-moon-missions,
author = {Wikipedia},
title = {{Wikipedia: List of missions to the Moon}},
url = {http://en.wikipedia.org/wiki/List{\_}of{\_}missions{\_}to{\_}the{\_}Moon},
urldate = {2015-06-04}
}
@misc{Hjorth2015,
author = {Hjorth, P G},
file = {:Users/gandalf/Library/Mobile Documents/com{\~{}}apple{\~{}}CloudDocs/-Sync/Mendeley/Hjorth/Hjorth - 2015 - A few Concepts from Analytical Mechanics, DTU (unpublished).pdf:pdf},
title = {{A few Concepts from Analytical Mechanics, DTU (unpublished)}},
year = {2015}
}
@misc{Copperheadtnp,
author = {Copperheadtnp},
keywords = {reddit-kerbal},
title = {{I was curious about the delta v requirements for different transfers. So I made this plot. At best, a bi-elliptic transfer will require 92{\%} of the delta v of a Hohmann transfer. : KerbalSpaceProgram}},
url = {http://www.reddit.com/r/KerbalSpaceProgram/comments/1ajru7/i{\_}was{\_}curious{\_}about{\_}the{\_}delta{\_}v{\_}requirements{\_}for/},
urldate = {2015-06-06},
year = {2013}
}
@misc{fig-ellipse,
author = {User), Stanmar (Wikipedia},
title = {{File:EllipseInPolarCoords2.svg - Wikimedia Commons}},
url = {http://commons.wikimedia.org/wiki/File:EllipseInPolarCoords2.svg},
urldate = {2015-06-06}
}
@book{Pisacane2005,
author = {Pisacane, Vincent L.},
edition = {2nd},
isbn = {978-0-19-516205-9},
pages = {828},
publisher = {Oxford University Press},
title = {{Fundamentals of Space Systems}},
year = {2005}
}
@misc{wiki-bi-elliptic,
author = {Wikipedia},
title = {{Wikipedia - Bi-elliptic transfer}},
url = {http://en.wikipedia.org/wiki/Bi-elliptic{\_}transfer{\#}Example},
urldate = {2015-06-06}
}
@misc{iss-worth,
author = {Minkel, J.R.},
title = {{Is the International Space Station Worth {\$}100 Billion?}},
url = {http://www.space.com/9435-international-space-station-worth-100-billion.html},
urldate = {2015-06-09}
}
@misc{nasa-sls,
abstract = {The largest, most powerful rocket booster ever built successfully fired up Wednesday for a major-milestone ground test in preparation for future missions to help propel NASA's Space Launch System (SLS) rocket and Orion spacecraft to deep space destinations, including an asteroid and Mars.},
author = {Ramsey, Sarah},
title = {{NASA's Space Launch System Booster Passes Major Ground Test}},
url = {http://www.nasa.gov/press/2015/march/nasas-space-launch-system-booster-passes-major-ground-test},
year = {2015}
}
@book{Taylor2009,
abstract = {An overall view of the vast spectrum of knowledge needed by practicing rocket scientists and engineers, Introduction to Rocket Science and Engineering presents the history and basics of rocket theory, design, experimentation, testing, and applications. It covers an array of fields, from advanced mathematics, chemistry, and physics to logistics, systems engineering, and politics. The text begins with a discussion on the discovery and development of rockets as well as the basic principles governing rockets and rocket science. It explains why rockets are needed from economic, philosophical, and strategic standpoints and looks at why the physics of the universe forces us to use rockets to complete certain activities. Exploring how rockets work, the author covers the concepts of thrust, momentum, impulse, and the rocket equation, along with the rocket engine, its components, and the physics involved in the generation of the propulsive force. He also presents several different types of rocket engines and discusses the testing of rocket components, subsystems, systems, and complete products. The final chapter stresses the importance of rocket scientists and engineers to think of the unusual, unlikely, and unthinkable when dealing with the complexities of rocketry. Taking students through the process of becoming a rocket scientist or engineer, this text supplies a hands-on understanding of the many facets of rocketry. It provides the ideal foundation for students to continue on their journey in rocket science and engineering.},
author = {Taylor, Travis S.},
edition = {1st},
isbn = {1420075292},
pages = {310},
publisher = {CRC Press},
title = {{Introduction to Rocket Science and Engineering}},
url = {https://books.google.com/books?id=dQHMBQAAQBAJ{\&}pgis=1},
year = {2009}
}
@misc{Okada2015,
abstract = {Ed Belbruno, a mathematician at NASA's Jet Propulsion Lab by day and an artist by night, pioneered a new way of space travel using canvas, paint and chaos theory. But no one believed in his work. Until one day, he had a chance to prove he was right.},
author = {Okada, Jacob Akira},
title = {{Painting the Way to the Moon}},
url = {http://www.paintingthewaytothemoon.com/ http://www.imdb.com/title/tt4294246/},
year = {2015}
}
@misc{universe-today-hiten,
author = {Williams, Matt},
title = {{Making the Trip to Mars Cheaper and Easier: The Case for Ballistic Capture}},
url = {http://www.universetoday.com/117615/making-the-trip-to-mars-cheaper-and-easier-the-case-for-ballistic-capture/},
urldate = {2015-06-08}
}
@misc{nasa-orion,
abstract = {NASA's Orion spacecraft continues on the agency's journey to Mars as engineers analyze data from the spacecraft's December flight test and make progress developing and building the spacecraft for its first mission atop NASA Space Launch System (SLS) heavy-lift rocket.},
author = {Garcia, Mark},
title = {{NASA's Orion Flight Test Yields Critical Data}},
url = {http://www.nasa.gov/content/nasa-s-orion-flight-test-yields-critical-data-as-engineers-improve-spacecraft-for-next},
year = {2015}
}
@misc{fig-hohmann-lti,
author = {"Aresv"},
title = {{File:Trans-lunar injection.svg - Wikimedia Commons}},
url = {http://commons.wikimedia.org/wiki/File:Trans-lunar{\_}injection.svg},
urldate = {2015-06-08}
}
@misc{nasa-hiten,
author = {NASA},
title = {{NASA - NSSDC - Spacecraft - Details}},
url = {http://nssdc.gsfc.nasa.gov/nmc/spacecraftDisplay.do?id=1990-007A},
urldate = {2015-06-08}
}
@book{Knudsen2002,
author = {Knudsen, Jens Martin and Hjorth, Poul G.},
edition = {3rd Editio},
isbn = {3-540-67652-X},
pages = {451},
publisher = {Springer-Verlag},
title = {{Elements of Newtonian Mechanics}},
year = {2002}
}