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Systems analysis of an ion-propelled orbital transfer vehicle /Brewster, Richard Wyatt, January 1990 (has links)
Thesis (M.S.)--Virginia Polytechnic Institute and State University, 1990. / Vita. Abstract. Includes bibliographical references (leaves 74-75). Also available via the Internet.
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Transferts orbitaux économiques. Cas des propulseurs à faible poussée.Genin, Y. January 1900 (has links)
Thèse--Liège. / Photocopy of typescript. Includes bibliographical references. Also issued in print.
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Laser engine simulation using pressure based navier-stokes solver /Youssef, Hazim S., January 1994 (has links)
Thesis (Ph. D.)--Virginia Polytechnic Institute and State University, 1994. / Vita. Abstract. Includes bibliographical references (leaves 267-273). Also available via the Internet.
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Transferts orbitaux économiques. Cas des propulseurs à faible poussée.Genin, Y. January 1900 (has links)
Thèse--Liège. / Photocopy of typescript. eContent provider-neutral record in process. Description based on print version record. Includes bibliographical references.
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Fuel-optimal control and guidance for low-and medium-thrust orbit transferGoodson, Troy D. 08 1900 (has links)
No description available.
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Piecewise-constant control strategies for use in minimum fuel aeroassisted orbital transfers /Page, Anthony Baker, January 1993 (has links)
Thesis (M.S.)--Virginia Polytechnic Institute and State University, 1993. / Vita. Abstract. Includes bibliographical references (leaves 78-80). Also available via the Internet.
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Parameter optimization of atmospheric skip trajectories for use in minimum fuel usage transfer orbits /Martell, Craig Alan, January 1991 (has links)
Thesis (M.S.)--Virginia Polytechnic Institute and State University, 1991. / Vita. Abstract. Includes bibliographical references (leaves 84-85). Also available via the Internet.
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Optimum transfers from circular orbits.Der, Gim Jew January 1978 (has links)
Thesis. 1978. Ph.D.--Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. / MICROFICHE COPY AVAILABLE IN ARCHIVES AND AERONAUTICS. / Vita. / Includes bibliographical references. / Ph.D.
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Analysis of the aerodynamic orbital transfer capabilities of a winged re-entry vehicle /Pienkowski, John P. January 2002 (has links) (PDF)
Thesis (M.S. in Space Systems Operations)--Naval Postgraduate School, September 2002. / Thesis advisor(s): Stephen A. Whitmore, Michael G. Spencer. Includes bibliographical references (p. 73-74). Also available online.
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Systems analysis of an ion-propelled orbital transfer vehicleBrewster, Richard Wyatt 30 December 2008 (has links)
A systems engineering approach was used to produce a preliminary design configuration for an ion-propelled orbital transfer vehicle system.
The four components of the system are: ground software, ground hardware, the orbital transfer vehicle and the space shuttle. The orbital transfer vehicle uses electrostatic propulsion to transfer payload satellites from a low earth orbit, to any other desired orbit.
The system maintenance concept, and a conceptual design are derived from the statement of need and the system operational requirements. The resulting design, maintainability, reliability and support requirements are discussed. A discussion of the feasibility of an ion propelled orbital transfer vehicle is included. / Master of Science
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