Global ETD Search

11	Time-domain finite elements in optimal control with application to launch-vehicle guidance Bless, Robert R. 05 1900 (has links) No description available. Control theory Mathematical optimization Launch vehicles (Astronautics)
12	Advanced guidance algorithms for the Ares V cargo launch vehicle Su, Shelly. January 2008 (has links) Thesis (M.S.)--University of Missouri-Columbia, 2008. / The entire dissertation/thesis text is included in the research.pdf file; the official abstract appears in the short.pdf file (which also appears in the research.pdf); a non-technical general description, or public abstract, appears in the public.pdf file. Title from title screen of research.pdf file (viewed on August 17, 2009) Includes bibliographical references.
13	A comparative investigation of a ground and air launch of LEO-bound microsatellites / Labib, Michael, January 1900 (has links) Thesis (M.App.Sc.) - Carleton University, 2007. / Includes bibliographical references (p. 151-156). Also available in electronic format on the Internet.
14	Legal aspects of launching and operating spacecraft Fiallos Pazmiño, Luis Fernando January 2003 (has links) No description available. Space law
15	Advanced Flight Control Issues for Reusable Launch Vehicles Bevacqua, Timothy R. 24 November 2004 (has links) No description available. Flight Control Controls Reusable Launch Vehicles
16	Concepts of operations for a reusable launch vehicle Rampino, Michael A. January 1900 (has links) Thesis--School of Advanced Airpower Studies, 1996. / Shipping list no.: 1998-0921-M. "September 1997." Includes bibliographical references. Also available via Internet from the Air University Press web site. Address as of 11/3/03: http://aupress.au.af.mil/SAAS%5FTheses/Rampino/rampino.pdf; current access is available via PURL.
17	ARCHITECTURE DISTRIBUTED ON EUROPEAN LAUNCHER Blondeau, Fabrice 10 1900 (has links) International Telemetering Conference Proceedings / October 20-23, 2003 / Riviera Hotel and Convention Center, Las Vegas, Nevada / Space vehicle telemetry requirements have evolved considerably over the past decade. More and more onboard data need to be acquired, not only for purposes of launch vehicle qualification in flight, but also for calibrating simulations. The flexibility required of the architecture has also changed the hardware considerably in order to fit into many different configurations without redoing the whole equipment development. EADS-LV accommodates these evolving needs and costs with a modular, distributed Telemetry channel architecture. This uses a single product line to meet the various needs ranging from the small launch vehicle to the heavy Ariane 5 vehicles. Telemetry architecture Distributed architecture Modular architecture Space launch vehicles
18	Reusable launch vehicles : crossroads between air and space law Vissepó, Varlin January 2003 (has links) No description available. Aerospace planes Space law
19	Distributed uncertainty analysis techniques for conceptual launch vehicle design McCormick, David Jeremy 08 1900 (has links) No description available. Computer simulation Uncertainty (Information theory)
20	Evaluation of advanced titanium matrix composites for 3rd generation reusable launch vehicles Craft, Jason Scott 08 1900 (has links) No description available. Metallic composites Fatigue Launch vehicles (Astronautics) Titanium alloys Fatigue

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