Ascent guidance for a winged boost vehicle
Name
20054837-MIT.pdf
Description
Full printable version
Size
7.37 MB
Format
Adobe PDF
Checksum (MD5)
6bf47a0267b9e5c3c262aa6b0d3f6f52
Author(s)
Corvin, Michael Alexander
Advisor(s)
Richard H. Battin, Gilbert S. Stubbs.
Date Issued
1988
Publisher
Massachusetts Institute of Technology
Description
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.
Includes bibliographical references.
Subjects
Aeronautics and Astronautics.
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
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.
Persistent DSpace Link