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dc.contributor.advisorJeffrey A. Hoffman and John Danis.en_US
dc.contributor.authorLanford, Ephraim Roberten_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2011-05-23T15:32:53Z
dc.date.available2011-05-23T15:32:53Z
dc.date.copyright2011en_US
dc.date.issued2011en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/62889
dc.descriptionThesis (S.M. in Technology and Policy)--Massachusetts Institute of Technology, Engineering Systems Division, Technology and Policy Program; and, (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2011.en_US
dc.descriptionThis electronic version was submitted by the student author. The certified thesis is available in the Institute Archives and Special Collections.en_US
dc.descriptionCataloged from student submitted PDF version of thesis.en_US
dc.descriptionIncludes bibliographical references (p. 126-136).en_US
dc.description.abstractIn comparison with conventional and other conceived approaches, hopper spacecraft offer unique advantages in exploring Solar System objects beyond Earth. The present work began with a survey - based on documents from the White House, Congress, NASA, and the international planetary science community - of exploration plans and objectives in the United States. The results are presented, and lead into a representative description of goals that might be enabled by hoppers. Relevant hopper attributes are then described in comparison to other vehicle types, and these vehicle characteristics are mapped to the exploration goals to show how hoppers can facilitate achievement of policy and science objectives. Specific examples are examined by formulating and analyzing a demonstrative and timely variety of model missions on Earth's Moon, Mars, and Saturn's moon Titan. These analyses use models for both hovering and ballistic hops to produce realistic values for hopper performance including mass, fuel consumption, trajectory characteristics, and basic spacecraft subsystem characteristics. In sum, planetary hopper technology is not for every mission, but generally offers paradigm-changing mobility and flexibility for small additional mass or development costs. Mission planners should evaluate hoppers for suitability to their exploration goals. Policy recommendations are offered toward this purpose.en_US
dc.description.statementofresponsibilityby Ephraim Robert Lanford.en_US
dc.format.extent136 p.en_US
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsM.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.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectEngineering Systems Division.en_US
dc.subjectTechnology and Policy Program.en_US
dc.subjectAeronautics and Astronautics.en_US
dc.titleUnique abilities of hopper spacecraft to enable national objectives for solar system explorationen_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.description.degreeS.M.in Technology and Policyen_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.contributor.departmentMassachusetts Institute of Technology. Engineering Systems Division
dc.identifier.oclc725945386en_US


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