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Jeffrey A. Hoffman. Michel, Wendelin X Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Massachusetts Institute of Technology. Department of Aeronautics and Astronautics 2011-08-18T19:14:26Z 2011-08-18T19:14:26Z 2010 2010 http://hdl.handle.net/1721.1/65292 745019960 Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2010. Page 98 blank. Cataloged from PDF version of thesis. Includes bibliographical references (p. 93-97). The utilization of rocket hoppers can provide a valuable means of obtaining enhanced mobility for planetary surface exploration missions. Hoppers offer higher exploration versatility than landers, rovers, or other surface exploration systems through their ability to quickly traverse difficult terrain in a variety of planetary environments. Furthermore, using a hover hop rather than a ballistic hop can provide many operational advantages. As the distance between target sites increases, the advantages of a single hopper compared to multiple landers decreases. However, in certain cases, in-situ resource utilization could overcome this problem. A detailed seven-phase hover hop model, simplified approximation formulas for lunar hops, and an optimization tool are presented in this thesis. With these, it becomes possible to quickly obtain optimized values for the vehicle mass, engine mass, and other mission parameters for a specified hopper mission. Results obtained from the application of a lunar hover hop model to realistic mission scenarios demonstrate the utility of hoppers for tasks relevant to future robotic and human exploration of the Moon. by Wendelin X. Michel. S.M. 98 p. eng Massachusetts Institute of Technology SD card contains supplementary materials. M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. http://dspace.mit.edu/handle/1721.1/7582 Aeronautics and Astronautics. Use and sizing of rocket hoppers for planetary surface exploration Thesis application/pdf Publication unknown unknown <Publication xmlns="https://www.openaire.eu/cerif-profile/1.1/" id="ec5617a7-635a-4de8-9064-e5134466a5f6"> <Type xmlns="https://www.openaire.eu/cerif-profile/vocab/COAR_Publication_Types">http://purl.org/coar/resource_type/c_1843</Type> <Language>eng</Language> <Title>Use and sizing of rocket hoppers for planetary surface exploration</Title> <PublishedIn> <Publication> </Publication> </PublishedIn> <PublicationDate>2010</PublicationDate> <Authors> <Author> <DisplayName>Michel, Wendelin X</DisplayName> <Affiliation> <OrgUnit> </OrgUnit> </Affiliation> </Author> </Authors> <Editors> </Editors> <Publishers> <Publisher> <DisplayName>Massachusetts Institute of Technology</DisplayName> <OrgUnit /> </Publisher> </Publishers> <License>http://dspace.mit.edu/handle/1721.1/7582</License> <Keyword>Aeronautics and Astronautics.</Keyword> <Abstract>The utilization of rocket hoppers can provide a valuable means of obtaining enhanced mobility for planetary surface exploration missions. Hoppers offer higher exploration versatility than landers, rovers, or other surface exploration systems through their ability to quickly traverse difficult terrain in a variety of planetary environments. Furthermore, using a hover hop rather than a ballistic hop can provide many operational advantages. As the distance between target sites increases, the advantages of a single hopper compared to multiple landers decreases. However, in certain cases, in-situ resource utilization could overcome this problem. A detailed seven-phase hover hop model, simplified approximation formulas for lunar hops, and an optimization tool are presented in this thesis. With these, it becomes possible to quickly obtain optimized values for the vehicle mass, engine mass, and other mission parameters for a specified hopper mission. Results obtained from the application of a lunar hover hop model to realistic mission scenarios demonstrate the utility of hoppers for tasks relevant to future robotic and human exploration of the Moon.</Abstract> <Access xmlns="http://purl.org/coar/access_right" > </Access> </Publication>