Entry vehicle performance analysis and atmospheric guidance algorithm for precision landing on Mars

Author(s)
Dierlam, Todd Allen
Thumbnail
DownloadFull printable version (5.390Mb)
Advisor
Richard H. Battin.
Terms of use
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
Metadata
Show full item record
Description
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1990.
 
Includes bibliographical references (leaves 167-168).
 
Date issued
1990
URI
http://hdl.handle.net/1721.1/42490
Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Publisher
Massachusetts Institute of Technology
Keywords
Aeronautics and Astronautics
Collections