Optimal escape trajectory from a high earth orbit by use of solar radiation pressure.
Name
04600132-MIT.pdf
Description
Full printable version
Size
4.1 MB
Format
Adobe PDF
Checksum (MD5)
b8778df3dbeab8e28c9d4065c116f2e7
Author(s)
Green, Andrew Joseph
Advisor(s)
Louis A. D'Amario and Donald C. Fraser.
Date Issued
1977
Publisher
Massachusetts Institute of Technology
Description
Thesis. 1977. M.S.--Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.
MICROFICHE COPY AVAILABLE IN ARCHIVES AND AERO.
Bibliography : leaves 51-53.
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.
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