- About
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The Global ETD Search service is a free service for researchers
to find electronic theses and dissertations. This service is
provided by the
Networked Digital Library of Theses and Dissertations.
Our metadata is collected from universities around the world. If you manage a university/consortium/country archive and want to be added, details can be found on the NDLTD website.
Search results
Showing 1 to 10 of 70 (0.056 seconds)Spelling suggestions: "subject:"rocket engine""
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Flow field investigation in pulse 1 motor of a two-pulse solid rocket motor /Qian, Xin, January 1990 (has links)
Thesis (M.S.)--Virginia Polytechnic Institute and State University, 1990. / Vita. Abstract. Includes bibliographical references (leaves 49-50). Also available via the Internet.
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| 2 |
3-D flow and performance of a rocket pump inducer at design and off-design flow rates /Doan, Andrew W., January 1994 (has links)
Thesis (M.S.)--Virginia Polytechnic Institute and State University, 1994. / Vita. Abstract. Includes bibliographical references (leaves 92-93). Also available via the Internet.
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| 3 |
Quasi-optimal steady state and transient maneuvers with and without thrust vectoring /Dwyer, Michael E., January 1993 (has links)
Thesis (M.S.)--Virginia Polytechnic Institute and State University, 1993. / Vita. Abstract. Includes bibliographical references (leaves 45-46). Also available via the Internet.
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| 4 |
Experimental method of analyzing stress intensity factors and singularity order in rocket motor geometry /Che-way, Chang, January 1990 (has links)
Thesis (Ph. D.)--Virginia Polytechnic Institute and State University, 1990. / Vita. Abstract. Includes bibliographical references (leaves 128-132). Also available via the Internet.
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| 5 |
Design and testing of a gas distribution method for pulsed inductive thrusterMiller, Robert E. Hartfield, Roy J., January 2008 (has links)
Thesis--Auburn University, 2008. / Abstract. Vita. Includes bibliographical references (p. 52-53).
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| 6 |
Thrust vectoring experiments with gas injectionSekhon, Kalwant Singh, 1938- January 1964 (has links)
No description available.
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| 7 |
The effect of departure from ideality of a multiply ionized monatomic gas on the performance of rocket engines /Perkins, John Noble, January 1963 (has links)
Thesis (Ph. D.)--Virginia Polytechnic Institute, 1963. / Vita. Abstract. Includes bibliographical references (leaves 54-56). Also available via the Internet.
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| 8 |
A numerical study of combined convective and radiative heat transfer in a rocket engine combustion chamber /Savur, Mehmet Koray. January 2002 (has links) (PDF)
Thesis (M.S. in Mechanical Engineering)--Naval Postgraduate School, December 2002. / Thesis advisor(s): Ashok Gopinath. Includes bibliographical references (p. 81-82). Also available online.
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| 9 |
The interaction between throttling and thrust vectoring of an annular aerospike nozzle a thesis /Imbaratto, David, Murray, William Russell. January 1900 (has links)
Thesis (M.S.)--California Polytechnic State University, 2009. / Mode of access: Internet. Title from PDF title page; viewed on September 23, 2009. Major professor: William R. Murray. "Presented to the faculty of the College of Engineering, California Polytechnic State University, San Luis Obispo." "In partial fulfillment of the requirements for the degree [of] Master of Science in Mechanical Engineering." "September 2009." Includes bibliographical references (p. 80).
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| 10 |
Hole-type aerospike compound nozzle thrust vectoring a thesis /Beebe, Stanley Ikuo. Murray, William Russell. January 1900 (has links)
Thesis (M.S.)--California Polytechnic State University, 2009. / Mode of access: Internet. Title from PDF title page; viewed on September 28, 2009. Major professor: William Murray, Ph.D. "Presented to the faculty of California Polytechnic State University, San Luis Obispo." "In partial fulfillment of the requirement for the degree [of] Master of Science in Mechanical Engineering." "September 2009." Includes bibliographical references (p. 49-50).
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